Minutes of the AIAA Structural Dynamics Technical … Fall... ·  · 2010-05-26Minutes of the AIAA Structural Dynamics Technical Committee Andrew Brown, Secretariat Fall Meeting,

Minutes of the AIAA Structural Dynamics Technical Committee Andrew Brown, Secretariat

Fall Meeting, Wright State University, Dayton, Ohio, October 19, 2005

Introduction The fall 2005 meeting of the AIAA Structural Dynamics Technical Committee was held at Wright State University in Dayton, Ohio, on October 19, 2005. Engineering faculty member Joseph Slater hosted the meeting. Upon arrival, all attendees were provided with a generous continental breakfast, and were each given beautiful University coffee mugs. In addition, all attendees had a table name card pre-prepared, which facilitated the meeting and note-taking substantially. Call to Order.

Sue Janssen, Committee Chair, called the meeting to order at 9:00 am. Engineering Dean Bor Jang then welcomed attendees. Joe Slater described the engineering program at Wright State briefly; it consists of 4 major departments and offers 9 majors, with both Masters and Ph.D, which are 5 or 6 years old. The engineering school can combine catalogs with the Air Force Institute of Technology and University of Dayton, which allows much broader offerings. It has 65 faculty members and is growing, expecting to add another 5 or 10 in the next few years. It consists of about 50% graduate students, which is a very high relative percentage. Mechanical Engineering graduates about 60-80/year, with a total of 350 engineering undergrads graduating. The department performs a lot of research with Delphi, Wright-Pat, and Lexus-Nexxus. It also has a lot of investment in “new technologies,” defined to be information technology (secretary’s note – how has IT managed to own the term “new technology” worldwide?). The university has a large proportion of non-traditional students. Finally, the university was actually founded by a donation of land from Wright-Paterson Air Force Base and so is surrounded by the base.

15 members in attendance Andrew Brown, Raymond Gordnier, Sue Janssen, Dexter Johnson, Hyoung-Man Kim, Donald Kunz, Kirit Patel, Dale Pitt, John Rogers, Suresh Shrivastava, Joseph Slater, Surya Surampudi, Paul Taylor, Carol Wieseman, Bruce Willis 5 members attending via telcon: Teresa Kinney, John Kosmatka, Stephanie Wilson, Chad Hebert, Guru Gusruswamy Also via telcon, Jim Ertzwieler (guest who has applied for TC membership) All attendees then introduced themselves, and gave their organization, professional interests, and pet’s name. A new member, Dexter Johnson from NASA/Glenn Research Center, was in attendance. His current focus is magnetic levitation for rotating machinery. A hard copy roster and the minutes from the Spring ’05 SDTC meeting were passed around for corrections as needed. A motion was made and passed to accept these minutes.

Subcommittee reports Awards

Sue Janssen in lieu of Peretz. The only award we’re involved in at the moment is the SDM award, which is pretty well established. There was a question about the Jefferson cup (student award), which the SDTC used to pay for it; Sue took an action to check into its status. She and Carol Stewart, AIAA Awards manager, describe it as follows:

- The Jefferson Goblet Award was established at the 20th Structures, Structural

Dynamics, and Materials Conference in St. Louis (secretary note: that’s 1980, I think. May I suggest that we eliminate the numbering of the SDM conference and just replace it with the year? Do we really care that this year’s conference is the 47th? Wouldn’t we rather let people know it occurred in 2006?) to encourage student engineers to publish and present the results of their research at a major AIAA technical symposium. It was established by the SDTC, specifically Harry Harcrow of Martin Marietta. The award is named in honor of Thomas Jefferson and a goblet he designed in 1788 was selected for presentation to each student recipient. The students are solicited from universities located in the United States. The award consists of a handmade Jefferson Goblet, a certificate of award as a corporate scholar, and a cash award of $500. Unfortunately, there have been few papers submitted in recent years. In 2005, though, there were quite a few papers submitted because the guidelines were changed to allow the advisor as a co-author. There was a considerable amount of discussion at the 2006 (excuse me, 47th) SDM organizing committee meeting about how to encourage student papers on structural dynamics topics. Dr. Don Kunz asked if the SDTC should resume sponsorship of the Jefferson Goblet. Mr. Ralph Tate motioned the committee make a vote. Dr. Peretz Friedmann seconded. After the initial vote, further discussion was requested. The final vote was unanimous for the AIAA SDM Organizing Committee to sponsor the Jefferson Goblet again. Sue believe’s the conference program committee includes a Student Papers Competition Chair and that person would be tasked with selecting a Jefferson Goblet recipient from the SDM Conference and announcing the name at the luncheon. AIAA HQ only provides the Goblet and includes it in the script for the award luncheon. Best papers for the past year are shown in Honors & Awards News on the web. If AIAA HQ is provided with the name of the 2005 Goblet recipient, that information will be included on the list of best papers.

Sue encouraged everyone to apply for membership upgrades. Peretz and she are

willing to support nominations. Award nominations are also open, and many of these are given thru AIAA. Sue encouraged people to go online and check it out, noting that many of the nominations need to be submitted by November. Conferences

Paul Taylor – The SDM ‘06 will be May 1-4 in Newport Rhode Island. It’s at Hyatt Regency – ($450 night without AIAA rate, $136 with, great deal!). Carlos Cesnik was our representative this year to the SDM organizing committee, assisted by John Kosmata. They were applauded by all for doing a great job. There were 201 total structural dynamics abstracts, including 9 student abstracts. The SDTC is in charge of 27 sessions, much more than previous year (21). There are 3 special sessions. 584 reviews were assigned, of which 98% were completed. 40 TC members participated as reviewers and 28 “friends of the TC” reviewed. We were shooting for about 82% acceptance (typically we have the lowest acceptance rate); it turned out to be about 80% acceptance. This year will be largest conference ever, with 600-700 attendees expected. There will be a “soft” deadline 1 month before, and a hard deadline 2 weeks before. If you wait until the week of the conference to submit your paper, then ????. They are going to enforce a “no paper, no podium” rule this year. Session chairs need to keep on people in sessions to get them to upload ahead of time. There was a discussion about how to move schedules around within session to account for no-shows. By early November, session chairs & times are established. The need for a drop down menu of sessions for reviewers to refer to was made. Suggestions for reviewing (conference administration system) are still being taken; please email these to the technical chair, Rajiv Naik. The Conference committee was very aggressive with AIAA to get them to take suggestions. Send your suggestions to Paul Taylor, who will consolidate them. Kathy Chemenvey is new AIAA contact for SDM. Carlos has sent out request volunteers to chair sessions; if you respond, John will assign you. Carlos and John made sure there aren’t overlaps of same author presentations, and that they have a break between their presentations.

SDM ’07 will be in Hawaii! It was the west’s turn, and Paul says as far as the hotel goes, Hawaii turned out to be significantly cheaper than Las Vegas or San Francisco, which were other potential sites. The AIAA was supposedly aggressive beforehand and asked quite a few organizations ahead of time about whether there would be a problem sending people to Hawaii, and no organization said there would be! The AIAA needs to distribute the list of people who they contacted so that potential attendees can hold their feet to the fire.

Hyoung-man brought up idea to have a “black-ball” list; people who are no-shows without any reason and don’t tell us. There was a discussion about no-shows. Carlos and John did try to take that into account as far as scheduling based on expected no-shows. In response to a suggestion that no-shows who notify AIAA ahead of time be left out of the schedule, Paul took action to really look into having schedule printed as late as possible so that there aren’t gaps in the session. The suggestion was that the schedule can be done at the last minute on a paper insert; it doesn’t have to be in formal brochure that requires a lot of lead time. There was also a suggestion to have daily updates available. Dale made suggestion of “no-podium, no presentation”, and also “no-show, no proceedings”. Joe suggested maybe requiring a partial required pre-registration for non-members to encourage their attendance. Another suggestion was to have a paper submission fee. Education

Chad Hebert, lead, couldn’t come to the meeting due to a last minute requirement to perform a ground vibration test at LaRC. Sue Janssen substituted and presented the status of the outreach project. She showed the introduction of the video that is on CD.

There is still a lot of work to be done by committee members and Media fusion, Inc., the vendor working with us. Some new work performed was the successful inclusion of John Kosmata’s experiments. The new CD has complete interviews with people about careers. The education committee found a bunch of interactive animations; pendulum, violin string, baseball bat –the user can change a property and see what happens. Sue wants everyone to walk through the latest version of the CD, which will be send out, and to add text. Sue then presented Teresa Kinney’s charts. The CD actually is now a DVD because of more space available, therefore all video will be included. The background has been developed well, but needs more side notes for things. Some problems developing animations and videos due to problems with compatibilities. Converting Dan Worth’s Java script stuff is very difficult and expensive; Sue asked about requesting AIAA to pay for conversion. The next version will be Mac compatible. Number of videos is growing substantially. Funding status: Mike Tinker found funding from NASA to finish this up; it has been allocated to task, but has been stalled because there’s no vehicle to get the money to Media Fusion (has to be sole source, etc). Should be happening “any time”. Will go after more AIAA funding in the meantime. Now format and links are mostly fixed.

Sue made a request to all TC members to provide text for all the blocks on the DVD; e.g., the SR71 “block” would like some “gee-whiz” facts about the video but more importantly, how it ties to structural dynamics. Sue has suggestions for who could provide the information, and Chad will send out the format again. There is a glossary of terms: e.g. buffeting. Hyoung-Man would like an example of what is being looked for. Surya offered a video on micro air vehicles; ones that fly like a bat, ones that do surveillance (these vehicles are only 5 inches long, and could fly into building like a bug). The priority is to get text. Holes in the DVD right now are helicopters and general aviation. Guideline is about 500 words. Media fusion will have a narration that’s a subset of the text. Target audience is high school seniors/college freshman – can have different layers. Sue believes we really need to tie in technical concepts more. Even the “beef” that was there was hard to get to, but it’s been fixed. Can definitely bring in outside people if they can help. Looking for text by Christmas holidays. Teresa, Sue & Chad telcon on this regularly. Would like to have it released by early next year; maybe have forum at SDM to present it. Could use it for no-show fillers. Once final product is available, could upgrade regularly. Will be distributed for nominal fee to cover reproduction costs and postage. Question raised whether copyright on it; a copyright would prevent it from being shown at Boeing. Liaison

Bruce Willis; not a whole lot going on. Structures; haven’t been able to get minutes. Only report is Adaptive Structures from Carlos - they have been putting out a book. Publications

Suresh; 2005 Year in Review article has been accepted and will be published. He thanked all the contributors. The article was originally too short (has to be between 575 words and 625 words), but after a last minute appeal he was able to get plenty of material. Suggestions for future: need more input from industry; would like names of

people to harass to help out. The article will include a photograph of a solar sail. Suresh is also starting the SDTC newsletter; a draft is in work, so please consider submitting an article. The newsletter will be a forum for information, education, and opinions. The AIAA will disseminate a hard copy for us. Secretariat

Andy Brown discussed the expert database, which will combine with the roster into one document; it may be different sheets in an excel file (sec. note – turned out to be a “linked directory database” type document, which automatically links an excel file with a word document). Sue will not provide the database itself to AIAA, but she’ll be the contact. A new roster will also be sent out. Discussion about updating the website – a suggested new template will be a photo roster, and there was discussion about emails on website, and how to keep from being used by spammers. Standards Working Group

No change from previous work; 1st stage, collection of model correlation requirements completed. 2nd stage will begin next year. Teresa has new task at her new job at NASA KSC (congratulations Teresa!) of examining effects of uncorrelated models, so this should help with the task. Technology Assessment

Hyoung-Man – thinking about updating structure of web site; Many of the websites we had been referring to are now behind firewalls, which really messes things up. Website: Sue - Harry Himmelblau, a world famous environments expert, has offered to put his extensive information on our site. He’ll be getting with Dan soon. Lots of discussion about best way to permanently keep information. Sue emphasized the importance of getting the website up-to-date, and will contact AIAA (again) about this issue, as well as contacting Dan Worth to see what he knows. Old business – Sue Janssen: - 41 total members in SDTC, with a good mix of industry, government, and academia. There has been a lot of interest in joining the committee. Nominations are due Nov. 1. Please encourage “young” (under 35) members to join; since they are associate members, there’s no limit to the number of them allowed on the committee. This is a good thing all around. - Stephanie Wilson will fly a SDTC American Flag aboard the next shuttle mission, STS-121, for us. Go Stephanie! New business - AIAA wants us to identify specific contributions to society that our field has made. It will be used through AIAA public policy, with Timothy Howard in charge. Sue showed a template for how they’d like us to write it up. Dale Pitt mentioned that our main contribution is stiffness and mass, without which the universe would not exist, so that’s a pretty big contribution. In a related manner, NASTRAN is a big contribution.

- Carol Wieseman brought up the Aeroelasticity Consortium, which has been organized by NASA Langley. They are preparing for two workshops (dates unknown). The first workshop will consist of leaders (vice-presidents) of industry, NASA, academia discussing how to set up technical consortiums, specifically considering the legal and financial issues, and won’t be tied just to Aeronautical Engineering. The second workshop will be on the technical level with about 20-30 participants, and the main purpose will be to brainstorm critical areas of the future. Please contact her if you’re interested in participating. - Next meeting; elections for chair; new appointment for secretary. Conclusion The meeting concluded at 12:00 noon, and a delicious catered lunch on the rooftop patio was provided by Wright State. The attendees then were given a free tour of the Air Force Museum nearby, with two retired generals serving as our personal guides! It was fantastic, and many thanks go to Joe Slater for setting it up.

11

Structural DynamicsStructural DynamicsTechnical Committee FallTechnical Committee Fall

MeetingMeeting19 October 200519 October 2005

9 am EDT - noon9 am EDT - noon

Wright State UniversityWright State UniversityDayton, OHDayton, OH

TeleconTelecon number: 303-977-1004, code 931604# number: 303-977-1004, code 931604#

22

Structural Dynamics Technical Committee Fall MeetingStructural Dynamics Technical Committee Fall Meeting19 October 200519 October 2005

AgendaAgenda 9:009:00 Welcome to DaytonWelcome to Dayton 9:309:30 Call to OrderCall to Order 9:459:45 Subcommittee ReportsSubcommittee Reports 10:4510:45 Old BusinessOld Business 11:1511:15 New BusinessNew Business 11:3011:30 AdjournmentAdjournment 12:0012:00 LunchLunch Air Force Museum TourAir Force Museum Tour

33

Call to OrderCall to Order

IntroductionsIntroductions–– Name, organization, professional interestsName, organization, professional interests–– SDTC roleSDTC role–– Do you have a pet? What is itDo you have a pet? What is it’’s name?s name?

AttendanceAttendance–– Initial the rosterInitial the roster–– Guests, add your contact information to the roster andGuests, add your contact information to the roster and

indicate if you wish to be included on our e-mailindicate if you wish to be included on our e-maildistributiondistribution

Approval of the spring meeting minutesApproval of the spring meeting minutes

44

Subcommittee ReportsSubcommittee Reports

–– Awards (Peretz Friedmann)Awards (Peretz Friedmann)–– Conferences (Paul Taylor)Conferences (Paul Taylor)–– Education (Chad Hebert)Education (Chad Hebert)–– Liaison (Bruce Willis)Liaison (Bruce Willis)–– Publications (Don Edberg)Publications (Don Edberg)–– Secretariat (Andy Brown)Secretariat (Andy Brown)–– Standards Working Group (Teresa Kinney)Standards Working Group (Teresa Kinney)–– Technologies (Hyoung-man Kim)Technologies (Hyoung-man Kim)–– Website (Dan Worth)Website (Dan Worth)

55

Awards SubcommitteeAwards Subcommittee

Current membersCurrent members–– Peretz Friedmann (Chair), Peretz Friedmann (Chair), InderjitInderjit Chopra, Chopra, ConorConor Johnson, John Johnson, John

KosmatkaKosmatka, Frank , Frank PaiPai

SDM AwardSDM Award MembershipMembership upgrades (online forms)upgrades (online forms)

–– http://www.aiaa.org/content.cfm?pageid=183http://www.aiaa.org/content.cfm?pageid=183

AwardAward nominations are opennominations are open–– http://www.aiaa.org/content.cfm?pageid=194http://www.aiaa.org/content.cfm?pageid=194

66

Conferences SubcommitteeConferences Subcommittee

Current membersCurrent members–– Carlos Cesnik, Carlos Cesnik, InderjitInderjit Chopra, Chopra, HyoungHyoung-Man Kim, Don Kunz, John-Man Kim, Don Kunz, John

Kosmatka, Rick Lind, Ramesh Malla, Fred Nitzsche, Frank Kosmatka, Rick Lind, Ramesh Malla, Fred Nitzsche, Frank PaiPai, Dale Pitt,, Dale Pitt,Charles Spiekermann, Paul Taylor (Chair), Firdaus Udwadia, CarolCharles Spiekermann, Paul Taylor (Chair), Firdaus Udwadia, CarolWieseman, Y.C. YiuWieseman, Y.C. Yiu

2006 SDM2006 SDM–– 1 - 4 May 2006 in Newport, Rhode Island (Hyatt Regency)1 - 4 May 2006 in Newport, Rhode Island (Hyatt Regency)–– SDTC Representative SDTC Representative –– Carlos Carlos CesnikCesnik–– SDTC Alternate Representative SDTC Alternate Representative –– John John KosmatkaKosmatka

77

47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics andMaterials Conference

SDM 2006 Planning Meeting

Structural Dynamics Session Status

Carlos E. S. CesnikAssoc. Prof. Aerospace Engineering

University of Michigan, Ann Arbor, Michigan

SDTC Fall Meeting, Dayton, Ohio12 October 2005

88

Structural Dynamics SubmittedStructural Dynamics SubmittedAbstractsAbstracts

Technical

Special 201 Total SD Abstracts Submitted201 Total SD Abstracts Submitted 9 Student Abstracts (2 redirected)9 Student Abstracts (2 redirected) 5 (before review assignment) +3 (from reviewers5 (before review assignment) +3 (from reviewers’’ recommendation) recommendation)

Redirected to other areasRedirected to other areas 4 Rejected (screening + 1 review)4 Rejected (screening + 1 review) 0 Returned for Revision0 Returned for Revision 3 Special Sessions3 Special Sessions

Special Sessions6%

Regular Sessions74%

Rejected16%

Transfer4%

99

Review ProcessReview Process

196 Abstracts reviewed and 193 retained196 Abstracts reviewed and 193 retained 584 Reviews assigned584 Reviews assigned

–– 3 per abstract3 per abstract–– 1 per 1 per ““rejectedrejected”” pre-screened abstracts pre-screened abstracts

(total of 4)(total of 4) 98% completed98% completed

–– Most of non-responded reviewers wereMost of non-responded reviewers werereplaced by an additional reviewerreplaced by an additional reviewer

Members of the Review TeamMembers of the Review Team–– All participants contacted and instructedAll participants contacted and instructed

on the review criteriaon the review criteria–– 40 TC Member Reviewers40 TC Member Reviewers–– 28 Friends of TC Reviewers28 Friends of TC Reviewers–– Several other Several other ““VolunteeredVolunteered”” Reviewers Reviewers

appointed within organizationappointed within organization3 reviews

87%

2 reviews11%

1 review2%

1010

0

5

10

15

20

25

30

35

40

45

0 1 2 3 4 5

Score

# o

f pap

ers

Scoring ProcedureScoring Procedure

Assigned number to the reviewAssigned number to the review Calculated the average scoreCalculated the average score Ranked all abstractsRanked all abstracts

Good

Avg

Bad

GoodAvgBad

83% of final list or 80% of total

Determined score for 82% cutoffDetermined score for 82% cutoff

Grade Policyr+ Strong Recommend 5r Recommend 4a Average 3rej Reject 1rej+ Strong Reject 0

Score Qty Acceptance Total5 3 2% 3

4.7 14 9% 174.5 5 11% 224.3 26 25% 484 42 47% 90

3.7 29 62% 1193.5 6 65% 1253.3 18 74% 1433 19 84% 162

2.7 6 87% 1682.3 3 89% 1712 4 91% 175

1.7 3 92% 1781.3 4 94% 1821 3 96% 185

0.7 2 97% 1870.3 3 98% 1900 3 100% 193

1111

# Title A bstract Folder N ote A uthor 1 A uthor 2 A uthor 3 A ffiliation RA RC r+ r a rej rej+ rev ws Average48713 Nonlinear random response of a clamped plate: a well-characterized experiment Acoustic loads This should be review ed w ith 48719 aboveG ordon H ollkam p AFR L 3 3 1 2 0 0 0 0 0 4.3 149360 Investigation of Acoustic Loading Due to Tones Using a STOVL Test Facility Acoustic loads R ussell Patience BAE System 3 3 1 2 0 0 0 0 0 4.3 248470 The Nonlinear Response of a Plate to Acoustic Loading: Predictions and Experiments Acoustic loads H ollkam p Beberniss G ordon AFR L 3 3 0 2 1 0 0 0 0 3.7 349388 Response of Plates Under Uniform Random Loads Unsynchronized in Time Acoustic loads C ould also be Structural dynam ics--platesD hainaut C heng M ei Em bry-R iddle, O ld D om inion 3 3 0 2 1 0 0 0 0 3.7 448710 Reduced Order Modeling of Random Response of Curved Beams using Implicit Condensation Acoustic loads Acoustics G ordon H ollkam p AFR L 3 3 1 1 1 0 0 0 0 4.0 548797 Active Alleviation of Gust Loads Using Special Control Surfaces Active C ontrol Karpel M oulin Feldgun Technion, EAD S Spain 3 3 0 3 0 0 0 0 0 4.0 648510 Non Linear Aeroelastic Response and Control of Supersonic Flapped 2-D Lifting Surfaces Active C ontrol C heck this one against a sim ilar paper by Librescu…M arzocca Librescu N a C larkson U niversity, Virginia Tech 3 3 0 2 1 0 0 0 0 3.7 749661 Robust Aeroelastic Control of 2-D Supersonic Flapped Lifting Surfaces Active C ontrol N a Librescu M arzocca Korea U niv, VPI 3 3 0 2 1 0 0 0 0 3.7 849791 Active Control of Non-Linear Aeroelastic Response Using Conformal Control Surfaces Active C ontrol C ould also be Aeroelasticity-nonlinearM arques M arqui C aixeta U SP Brazil 3 3 0 2 1 0 0 0 0 3.7 949547 Nonlinear Flutter and Time-delayed Feedback Control of a 2-D Supersonic Flapped Wings Active C ontrol Aeroelasticity-nonlinear C hen M arzocca Librescu U niversity of Western O ntario, C larkson, VPI3 3 0 2 1 0 0 0 0 3.7 1049848 Control Structure Interaction Testbed: Passive Isolation, Simulation & Test Active C ontrol This should be review ed along w ith 49852Brennan N orthrop G rum m an Space Technology3 3 0 3 0 0 0 0 0 4.0 1150918 Concurrent Optimal Design of Piezoelectric Actuators and Controller for Active Vibration Control Active Control Joshi Mujumdar IIT, Bombay 3 3 0 2 0 1 0 0 0 3.0 1250982 Analytical-Experimental Study on Using Different Control Surfaces to Alleviate Dynamic Loads Aeroelastic design Kuzmina Ishmuratov Zichenkov TsAGI 3 3 1 2 0 0 0 0 0 4.3 1350860 Maneuver Load Analysis of an Over-Determined Trim System Using a CFD Code Aeroelastic design Aeroelastic optimizationRaveh Technion 3 3 2 1 0 0 0 0 0 4.7 1448681 Shape Sensitivities Of Minimum-State Unsteady Aerodynamics Approximations Aeroelastic design M or Livne U niv. Washington 3 3 1 2 0 0 0 0 0 4.3 1548761 Design Optimization Studies of Strain Actuated Flight Vehicles Aeroelastic design Jackson Livne Sterling D ynam ics, U niv Washington3 3 1 2 0 0 0 0 0 4.3 1649546 Aeroelastic Behavior of a Non-Rigidizable Inflatable UAV Wing Aeroelastic design Aeroelastic design R endall Chang Marzocca Im perial C ollege, C larkson 3 3 1 1 1 0 0 0 0 4.0 1748714 An Experimental and Numerical Aeroelastic Analysis of a Morphing Wing Micro Air Vehicle Aeroelastic design Stanford Abdulrahim Lind U niv Florida 3 3 0 2 1 0 0 0 0 3.7 1851164 Linear Modeling of Highly Aeroelastic Control Effectors Aeroelastic design Griffin SwRI 3 3 1 1 0 1 0 0 0 3.3 1948211 (Student Paper) Flutter of partially rigid cantilevered plates in axial flow Aeroelasticity Panel Flutter De Breuker Abdalla GÄurdal Delft 3 3 1 2 0 0 0 0 0 4.3 2049317 Finite Element Time Domain - Modal Formulation for Nonlinear Flutter of Composite Curved Panels Aeroelasticity Panel Flutter Azzouz M ei O ld D om inion 3 3 0 3 0 0 0 0 0 4.0 2148330 Flutter Analysis of Viscoelastic Sandwich of Cylindrical Panels in Supersonic Flow Aeroelasticity Panel Flutter Khudayarov private 3 3 0 1 2 0 0 0 0 3.3 2249454 Aerothermoelastic Stability of Composite Aircraft Wings Subjected to Heat Inputs Aeroelasticity-linear aerotherm oelasticity Trapani M astroddi Librescu R om a La Sapienza, VPI 3 3 1 2 0 0 0 0 0 4.3 2349371 Evaluation of Prediction Methods for MDOF Aircraft Aeroelasticity-nonlinear LC O Vio D im itriadis C ooper U niv M anchester 3 3 0 1 2 0 0 0 0 3.3 2449867 Nonlinear Aeroelastic Studies on a Folding Wing Configuration with Free-play Hinge Nonlinearity Aeroelasticity-nonlinear Lee C hen ZO N A 3 3 0 1 2 0 0 0 0 3.3 2550891 (Student Paper) Aeroelastic Analysis of an Airfoil with a Hysteresis Non-linearity Aeroelasticity-nonlinearfree play Guo Yang Northwestern Polytechnical University, China3 3 0 0 3 0 0 0 0 3.0 2649765 Aeroelastic Response and Robust Control of Aircraft Wings Modeled as Thin-Walled Beams Aeroservoelasticity linear Librescu Q in N a VPI, Korea U niv 3 3 0 2 0 1 0 0 0 3.0 2748646 Modeling of Aeroservoelastic Systems with Nonlinear Strain Actuation Aeroservoelasticity M olin Karpel Technion 3 3 1 2 0 0 0 0 0 4.3 2848593 Reduced-Size Aeroservoelastic Modeling and LCO Simulations with Structurally Non-Linear Actuators Aeroservoelasticity G old Karpel Technion 3 3 1 1 1 0 0 0 0 4.0 2949646 Development of Aeroservoelastic Analytical Models of a Sensorcraft Wind-Tunnel Model Using Measured Data Aeroservoelasticity Sensorcraft Silva Vartio Scott N ASA LaR C , N G C 3 3 0 3 0 0 0 0 0 4.0 3049636 Aeroservoelasticity Interactions Studies on a Business Aircraft Aeroservoelasticity Botez D inu C otoi U niversité du Q uébec 3 3 0 2 1 0 0 0 0 3.7 3148649 Characterization of Methods for Computation of Aeroservoelastic Systems Response to Gust Excitation Aeroservoelasticity Azoulay Karpel Technion 3 3 1 1 1 0 0 0 0 4.0 3248508 Numerical Simulation of the Buffet of a Full Span Delta Wing at High Angle of Attack C om putational AeroelasticityAeroelasticity-nonlinear Attar G ordnier AFR L 3 3 1 2 0 0 0 0 0 4.3 3349754 Dynamic Aeroelasticity of Flexible Slender Wings in Compressible Flow C om putational AeroelasticityC ould also be Aeroelasticity-nonlinearC esnik C him akurthi U niv M ichigan 3 3 1 2 0 0 0 0 0 4.3 3449829 Parallel Algorithm for Fully Nonlinear Aeroelastic Analysis C om putational AeroelasticityC ould also be Aeroelasticity-nonlinearG argoloff Strganac Beran Texas A&M , AFR L 3 3 0 3 0 0 0 0 0 4.0 3549563 Flutter Prediction by Euler Method Coupled with Boundary Layer Model Computational aeroelasticity Lai Koh Tsai National University of Singapore3 3 0 2 1 0 0 0 0 3.7 3649567 Treatment of Complex Configurations for Flutter Calculations C om putational AeroelasticityM esh/grid interpolation R am puraw ala Badcock Woodgate U niversity of G lasgow 3 3 0 2 1 0 0 0 0 3.7 3749640 Transonic Flutter Prediction of Supersonic Jet Trainer with Various External Store Configurations C om putational Aeroelasticity In Lee Kw on Jong-Yun Kim KAIST, Seoul N ational, etc. 3 3 0 1 2 0 0 0 0 3.3 3849551 Comparative Analysis of Computational Methods for Limit-Cycle Oscillations C om putational AeroelasticityLC O G opinath Beran Jam eson AFR L, Stanford 3 3 0 2 0 1 0 0 0 3.0 3949817 Experimental and Analytical Estimation of Loss Factors by the Power Input Method D am ping Experim ental Structural D ynam icsLiu Ew ing U niv Kansas 3 3 2 1 0 0 0 0 0 4.7 4051043 Damping Characteristics of Viscoelastically Constrained Fibrous Carbon Strands Damping Vasudeva Kapania Cliff VPI 3 3 2 1 0 0 0 0 0 4.7 4149468 On Estimating the Loss Factors of Plates with Constrained Layer Damping Treatments D am ping Torvik R unyon AFR L 3 3 1 2 0 0 0 0 0 4.3 4251052 Efficient Frequency Response Analysis of Structures with Viscoelastic Materials Damping Swenson Bennighof The University of Texas at Austin3 3 0 1 2 0 0 0 0 3.3 4349878 An Iterative Finite Element Approach to Modeling Damping Coatings D am ping R unyon Justice AFR L, U TC 3 3 0 2 0 1 0 0 0 3.0 4451045 Nonlinear Deformations of Flapping Wings on a Micro Air Vehicle Dynamics Barut Madenci The University of Arizona 3 3 2 1 0 0 0 0 0 4.7 4549759 Validation of a Generalized Direct Approach for Analysis of Multibody Dynamic Systems D ynam ics Kunz AFIT 3 3 0 2 1 0 0 0 0 3.7 4650954 Practical Large-Motion Modeling of Geometrically Complex Flexible Vehicles Dynamics Nonlinear structural dynamicsMcTavish Davidson Ryerson University, Toronto3 3 0 1 2 0 0 0 0 3.3 4751165 Dynamics of Insect-Based Flapping Wings: Inertial Loads Validation Dynamics Flapping wings MAVSingh Chopra Univ Maryland 3 3 1 1 0 1 0 0 0 3.3 4849387 Simulation of a Moving, Elastic Beam using Hamilton's Weak Principle D ynam ics Strut dyn beam s Leigh Kunz AFIT 3 3 0 2 1 0 0 0 0 3.7 4949606 Computational Modeling of Highly Flexible Membrane Wings in Micro Air Vehicles Dynamics N onlinear m em brane Seshaiye G ordnier Texas Tech U niversity, AFR L 3 3 1 1 1 0 0 0 0 4.0 5049537 Nonlinear Aeroelastic Modeling and Experiments of Flexible Wings Experim ental Aeroelasticity R om eo Frulla M arzocca Polytecnico di Torino, C larkson 3 3 0 2 1 0 0 0 0 3.7 5149941 Nonlinear Behaviors and Control Surface Interaction Effects of the Active Aeroelastic Wing Wind Tunnel Model Experim ental Aeroelasticity H eeg N ASA LaR C 3 3 1 2 0 0 0 0 0 4.3 5249802 Higher Order Statistical Signal Processing Studies on the Impact of Icing in Aircraft Stability, Control and Aeroelastic Behavior Experim ental AeroelasticityIcing test Stearm an G oldstein Endruhn U niv Texas Austin 3 3 0 2 1 0 0 0 0 3.7 5349740 Experiments on Bending-Torsion Nonlinear Flutter of the Medium-Aspect-Ratio Wing Experim ental Aeroelasticity H arash Yadykin Abram ovich Technion 3 3 0 1 2 0 0 0 0 3.3 5450979 Extracting Dynamic Aerodynamic Loads from Optical Deformation Measurements Experimental aeroelasticity Roy Liu Britcher Old Dominion, West Michigan3 3 3 0 0 0 0 0 0 5.0 5548404 Wind Tunnel Aeroelastic Testing of a Three Surface Demonstrator Experim ental aeroelasticity R icci Scotti Politecnico di M ilano 3 3 0 2 1 0 0 0 0 3.7 5650970 Flight Flutter Testing of a Transport Aircraft with Wing Mounted Store Suspension - Lessons Learned Experimental aeroelasticityFlight testing KAYRAN Middle East Technical University, TURKEY3 3 0 2 1 0 0 0 0 3.7 5748547 Selection of a Location with Additional Mass and Stiffness in Component Modal Tests Experim ental structural dynam ics M isaw a M atsuo Shizuoka U niversity, Japan 3 3 0 2 1 0 0 0 0 3.7 5849332 Noise Separation Experiment for Flexible Structures Using Variable Mass Experim ental structural dynam ics Senba Furuya Tokyo Institute of Technology 3 3 0 3 0 0 0 0 0 4.0 5950827 Modeling of Ground Vibration Testing for Highly Flexible Aircraft Experimental structural dynamicsStructural dynamics Chang Hodges Georgia Tech 3 2 0 2 0 0 0 0 0 4.0 6049723 (Student Paper) Experimental Dynamic Response of a Munition to a Low Pressure Airbag Experimental structural dynamicsAirbag dynamics Dreher Canfield Maple AFIT 3 3 1 1 0 0 1 0 0 3.0 6151006 Experimentally Quantifying the Dynamic Response of Bolted Lap Joints Experimental structural dynamicsbold joints Page Slater Pettit Wright State University, United States Naval Academy3 2 0 1 1 0 0 0 0 3.5 6250989 (Student Paper) Aeroelastic Response of Highly Flexible Flying Wings HALE UAV Su Cesnik Univ Michigan 3 3 2 1 0 0 0 0 0 4.7 6349757 Nonlinear Aeroelastic Analysis of a Wing in Nonzero Trims HALE UAV Aeroelasticity-nonlinear N ichkaw de Strganac Beran Texas A&M , AFR L 3 2 1 1 0 0 0 0 0 4.5 6449818 Nonlinear Flight Dynamics and Gust Response of Highly Flexible Aircraft H ALE U AV G ust response Patil H odges VPI, G eorgia Tech 3 3 2 0 1 0 0 0 0 4.3 6548794 Static and Dynamic Aeroelasticity of Joined Wing Configurations H ALE U AV D em asi Livne U niv Washington 3 3 0 3 0 0 0 0 0 4.0 6649884 Time Domain Nonlinear Aeroelastic Analysis for HALE Wings H ALE U AV Wang C hen Patil ZO N A, VPI 3 3 0 3 0 0 0 0 0 4.0 6751008 Stability, Control, and Simulation of High-Altitude-Long-Endurance UAVs HALE UAV Aeroelasticity-nonlinearTuzcu Marzocca Cestino The University of Alabama, Clarkson, Politecnico di Torino3 3 0 0 3 0 0 0 0 3.0 6851066 Transonic Limit Cycle Flutter of High-Aspect-Ratio Swept Wings HALE UAV LCO Bendiksen UCLA 3 3 2 1 0 0 0 0 0 4.7 6948378 Robust Bird-Strike Modeling Based on SPH Formulation Using LS-DYNA Im pact loading responseC om putational structural dynam icsG oyal H uertas Vasko U niversity of Puerto R ico, P&W 3 3 1 0 2 0 0 0 0 3.7 7049933 A Large Deflection Model for Thin, Rectangular Plates Subjected to Blast Loading Impact loading responseblast Florek Benaroya Rutgers University 3 3 2 0 1 0 0 0 0 4.3 7149883 A Consistent Configuration Formulation of Continuum Damage Mechanics Based Lagrangian Hydrodynamic Computational Framework for 3D High- and Hypervelocity Impact/Damage/Penetration Analysis Im pact loading response Zhou Sha Tam m a Arm y H igh Perform ance C om puting R esearch C enter (AH PC R C )4 3 0 1 2 0 0 0 0 3.3 7249526 Experimental and Finite Element Analysis of Preloaded Bolted Joints Under Impact Loading Im pact loading response O ’Toole Karpanan Feghhi U niversity of N evada Las Vegas3 3 0 3 0 0 0 0 0 4.0 7348452 Cannel Section Short Column With Fixed Ends Under Axial Impact Load Im pact loading response Shoji M inegishi Aoki Japan Aerospace Exploration Agency, U niversity of Tokio3 3 0 1 2 0 0 0 0 3.3 7449555 Accuracy Improvement of Water Impact Analysis for Airplane Ditching Im pact loading responseD itching loads Ishihara Shoji M inegishi Japan Aerospace Exploration Agency3 3 1 1 0 1 0 0 0 3.3 7548606 Simulation of Landing Events for an Unconventional UAV Landing Gear System Using Transient Dynamics Approach Im pact loading response N guyen M ak Panza G eneral Atom ic Aeronautical System s3 3 0 0 3 0 0 0 0 3.0 7649323 An Investigation of the Sensitivity of F-16 Fighter Limit Cycle Oscillations to Uncertainties LC O Thom as D ow ell D enegri D uke, SEEK EAG LE 3 3 1 2 0 0 0 0 0 4.3 7749472 Analysis of Store Effects on Limit-Cycle Oscillation LC O Parker M aple Beran AFIT, AFR L 3 3 1 2 0 0 0 0 0 4.3 7848295 Limit Cycle Oscillation Prediction of Asymmetric External Store Configurations using Neural Networks LC O D aw son M axw ell SEEK EAG LE 3 3 0 3 0 0 0 0 0 4.0 7948807 Suppression of Aeroelastic Instability with a Nonlinear Energy Sink: Theoretical Basis LCO Nonlinear AeroelasticityLee Vakakis Bergman University of Illinois at Urbana-Champaign3 3 0 3 0 0 0 0 0 4.0 8049756 Suppression of Limit Cycle Oscillations With a Nonlinear Energy Sink: Experimental Results LC O Experim ental AeroelasticityH ill Strganac N ichkaw de Texas A&M , U IU C 3 3 0 3 0 0 0 0 0 4.0 8150872 Flight-Loads Effects on Free-play Induced Limit Cycle Oscillation LCO Chen Lee ZONA 3 3 0 3 0 0 0 0 0 4.0 8251020 Nonlinear Characteristics of a Transient Response of NATA LCO Spectral analysis Chabalko Mook Silva VPI, NASA LaRC 3 3 0 2 1 0 0 0 0 3.7 8350871 Vibration Damping of Cylindrical Shells using Low-Density, Granular Materials Particle Damping Verdirame Nayfeh MIT 3 3 2 1 0 0 0 0 0 4.7 8451163 New Particle Damping Applications Particle Damping Simonian NGC 3 2 1 1 0 0 0 0 0 4.5 8548767 Macromodel Characterisation and Application of Particle Dampers to Vibrating Structures Particle damping Wong Rongong Univ Sheffield 3 3 0 3 0 0 0 0 0 4.0 8651087 New Particle Damping Applications Particle damping Simonian Brennan NGC 3 3 1 1 1 0 0 0 0 4.0 8749967 Particle Impact Damping in the Horizontal Plane Particle D am ping Kinra Witt Texas A&M 3 3 1 0 2 0 0 0 0 3.7 8848584 Optimized Non-Obstructive Particle Damping (NOPD) Treatment for Composite Honeycomb Structures Particle D am ping Panossian P&W 3 3 0 2 0 1 0 0 0 3.0 8951240 The particle damping phase diagram for constrained cavities Particle damping Sauena Poschel Schwager U niversitat R ovira i Virgili, Spain 3 3 1 0 1 1 0 0 0 3.0 9048405 Application of Higher-Order Harmonic Balance to Non-Linear Aeroelastic Systems R educed order m odelingR educed order m odel D im itriadis Am uyedo C ooper U niv M anchester 3 3 0 2 1 0 0 0 0 3.7 9150911 Flutter Simulation and Prediction with CFD-Based Reduced-Order Model R educed order m odelingC om putational aeroelasticityLai Won Koh N ational U niversity of Singapore 3 3 1 1 1 0 0 0 0 4.0 9249832 CFD-Based Discrete Gust Response Analysis of Elastic Wings Reduced order modelingG ust response Zaide R aveh Technion 3 3 0 3 0 0 0 0 0 4.0 9349576 A Reduced Damping Model Derived from CFD Based Aeroelastic Simulations Reduced order modeling Woodgate Badcock University of Glasgow 3 3 2 1 0 0 0 0 0 4.7 9449469 Unified Rational Function Approximation Formulation For Aeroelastic And Flight Dynamic Analysis R educed O rder M odelingFlight dynam ics Baldelli C hen Panza ZO N A, G eneral Atom ics 3 3 1 2 0 0 0 0 0 4.3 9550965 Nonlinear Aeroelastic Analysis Using a CFD-Based State Space ROM Reduced order modeling Munteanu Rajadas Chattopadhyay Arizona State 3 3 1 1 0 1 0 0 0 3.3 9649758 Simultaneous Vibration Reduction and Performance Enhancement in Rotorcraft Using Actively Controlled Flaps R otorcraft Friedm ann Liu Kim U niv M ichigan 3 2 2 0 0 0 0 0 0 5.0 97

50756 Prediction of Helicopter Servo Loads During Unsteady Maneuvers Using Modified UMARC with Multibody Analysis Rotorcraft Abhishek Chopra Univ Maryland 3 3 2 1 0 0 0 0 0 4.7 9849814 Global Control of Helicopter Vibrations using a Semi-active Vibration Control System R otorcraft H ugin H atch Q inetiQ 3 2 1 1 0 0 0 0 0 4.5 9951088 Vibratory Loads Prediction for Designing Active Twist Rotor Rotorcraft Chimakurthi Thepvongs Cesnik Univ Michigan 3 2 1 1 0 0 0 0 0 4.5 10050090 Time and Frequency Domain Analysis of Whirl Flutter Stability in Tiltrotor Aircrafts R otorcraft Tilt rotor Kim Shin Kim Seoul N ational, Boeing 3 2 1 0 1 0 0 0 0 4.0 10151041 Nonlinear Flexible Multibody Dynamic Analysis of Rotor Blades with a Trailing Edge Flap Rotorcraft Das Barut Straub The University of Arizona, Boeing Mesa3 2 0 2 0 0 0 0 0 4.0 10248365 Rotor Blade Dynamic Stall Model and Its Influence on Airfoil Response R otorcraft Laxm an Venkatesan IIT Kam pur 3 2 0 1 1 0 0 0 0 3.5 10349545 Novel Attenuation Method of Transmitted Sound into Rocket Faring using Energy-Harvesting Technique Space loads and dynam ics M akihara O noda M inesugi JAXA, Japan 3 3 0 2 0 1 0 0 0 3.0 10449836 Shuttle-ISS Detailed Test Objective: Model Correlation - Development and Implementation Space loads and dynamics Bartkowicz McNeill Grygier Boeing, NASA Johnson 4 3 2 1 0 0 0 0 1 4.7 10549482 Natural Frequencies of an Innovative Space Based Radar Antenna by Continuum Modeling Space loads and dynam ics Salehian C liff Inm an VPI 3 3 1 1 1 0 0 0 0 4.0 10651334 Nonlinear Dynamic Failure Analysis of Truss Structures Atnormal and Elevated Temperatures Space loads and dynamicsTruss at elevated temperatureM alla Agarwal U niversity of C onnecticut 4 2 0 1 1 0 0 1 0 3.5 10751054 Parametric Buckling Analysis of Tape Springs Space loads and dynamicsBuckling Silver Hinkle Peterson Univ Colorado Bolder 3 2 0 2 0 0 0 0 0 4.0 10849981 Alternative Techniques for Developing Dynamic Analysis Computer Models of The International Space Station and Orbiter Repair Maneuvers Spacecraft Loads and D ynam ics G randa N guyen C alifornia State U niversity, N ASA Johnson3 3 1 0 1 1 0 0 0 3.0 10948379 Computational Dynamics in Design Optimization Special Session C om putational Structural D ynam icsVanderplaats Vanderplaats R esearch & D evelopm ent, Inc.3 3 1 2 0 0 0 0 0 4.3 11049394 Frequency Response Analysis of Complex Structures: Issues, Trends and Recent Developments Special Session C om putational Structural D ynam icsBennighof U niversity of Texas at Austin 3 3 1 1 1 0 0 0 0 4.0 11149515 Using Load-based Ritz Vectors for Dynamic Analysis of Structures Special Session C om putational Structural D ynam icsR ose M acN eal G roup 3 3 0 2 1 0 0 0 0 3.7 11249949 The state of the art in large scale, accurate eigenvalue computations Special Session C om putational Structural D ynam icsKom zsik U G S 3 3 1 0 2 0 0 0 0 3.7 11349792 Sustaining and Disruptive Technologies in Computational Structural Dynamics Special Session C om putational Structural D ynam icsAlvin Sandia N ational Laboratories 3 3 1 0 1 1 0 0 0 3.0 11450874 Geometrically-Exact, Intrinsic Theory for Dynamics of Moving Composite Plates and Shells Struc dyn shells plates and shells Hodges Yu Patil Georgia Tech, VPI 3 3 1 2 0 0 0 0 0 4.3 11549452 Dynamics of Microstructured Shells with Thickness Extension Struc dyn shells Polli M astroddi M orino U niversit!a degli Studi di R om a \La Sapienza"3 2 0 2 0 0 0 0 1 4.0 11649533 Localized Magnetoelastic Bending Vibration of an Electroconductive Elastic Plate Struc dyn shells Belubekyan G hazaryan M arzocca N ational Academ y of Sciences of Arm enia, C larkson3 3 0 2 1 0 0 0 0 3.7 11748058 Free Vibrations of Centrally Bonded Symmetric Lap Joint (or Symmetric Doubler Joint) with a Gap in Mindlin Plates or Panels Struc dyn shells plates Yuceoglu G üvendik M iddle East Technical U niversity, Turkey3 3 0 1 2 0 0 0 0 3.3 11849734 Free Vibration of Doubly-Curved Sandwich Panels with Laminated Face Sheets Struc dyn shells H ause Librescu M innesota State, VPI 3 3 0 3 0 0 0 0 0 4.0 11950956 Dynamic response of isotropic and composite plates under electromagnetic field Struc dyn shells Kumar Zhupanska Sierakowski Univ Florida, AFRL/Eglin 3 3 0 2 1 0 0 0 0 3.7 12048059 Free Transverse Vibrations Response of Integrally Stiffened Plate or Panel Systems with a Central Plate Stiffener Struc dyn shells Yuceoglu G uvendik Tuç M iddle East Technical U niversity 3 3 0 2 0 1 0 0 0 3.0 12148608 A Reduction Method for Finite Elements Nonlinear Dynamic Analysis of Shells Struct dynam ics C om putationalR educed order m odel Tiso Abdalla Jansen D elft U niversity of Technology 3 3 2 1 0 0 0 0 0 4.7 12250978 (Student Paper) Modified Generalized Alpha Method for Integrating Governing Equations of Very Flexible Aircraft Struct dynamics ComputationalHALE UAV Scheares Cesnik Univ Michigan 3 3 1 2 0 0 0 0 0 4.3 12349466 A Hermite High-Order Finite Element in Structural Dynamics Struct dynamics Computational M O R IN O C ETTA U niversit̀a“R om a Tre”, R om a 3 3 1 1 0 1 0 0 0 3.3 12451201 Accurate Structural Dynamic Modeling of the Hunter UAV Using Ground Vibration Testing Structural dynamicsReduced order modelKosmatka Valdes UCSD, NGC 3 3 2 1 0 0 0 0 0 4.7 12547788 Dynamic Snap Through Response of Thin-Walled Structures by a Reduced Order Method Structural dynam ics R educed order m odel R izzi Przekop N ASA LaR C , N IA 3 2 1 0 1 0 0 0 0 4.0 12650959 Component Effective Modal Mass Strut dyn beams Reduced order modelingMajed Henkel Applied Structural Dynamics, Inc.3 3 0 1 2 0 0 0 0 3.3 12748719 Finite Element Analysis of Beams with Nonlocal Foundations Strut dyn beam s Lei Frisw ell Adhikari N ational U niv of D efense Tech, PR C , U niversity of Bristol3 3 1 1 1 0 0 0 0 4.0 12851039 Energy-consistent, Galerkin approach for the nonlinear dynamics of beams using mixed, intrinsic equations Strut dyn beams Patil Althoff VPI 3 3 1 1 1 0 0 0 0 4.0 12950718 Dynamic Stability of Damped Laminated Composite Beams Subject to Subtangential Loads Strut dyn beams Goya Mercury University of Puerto Rico 3 3 1 2 0 0 0 0 0 4.3 13050977 Dynamics of Thin-walled Composite Aircraft Wings Carrying External Stores Strut dyn beams Kwon Librescu Song VPI 3 3 0 3 0 0 0 0 0 4.0 13149352 Dynamic Analysis of a Three-layered Sandwich Beam using Theory and Experiment Strut dyn beam s Banerjee N juguna C heung C ity U niversity, L 3 3 0 1 2 0 0 0 0 3.3 13248806 Spectral Element Modeling and Analysis of an Axially Moving Thermoelastic Beam-Plate Strut dyn beam s Spectral Analysis Kw on Lee Inha U niversity, Korea 3 3 1 2 0 0 0 0 0 4.3 13349330 Spectral Analysis Method for the Spectral Element Models Strut dyn beam s Spectral Analysis C ho Lee Inha U niversity, Korea 3 3 0 1 2 0 0 0 0 3.3 13450805 SHARCS Project: Modal Parameters Identification of Smart Spring/Helicopter Blade System System ID Rotorcraft Coppotelli Marzocca Nitzsche University of Rome “La Sapienza”, Clarkson, Carlson3 2 1 0 1 0 0 0 0 4.0 13551202 Development of an In-Flight Structural Health Monitoring System for Composite Unmanned Aircraft System ID SHM Kosmatka Oliver UCSD 3 3 3 0 0 0 0 0 0 5.0 13649396 Identification of Nonlinear Aeroelastic and Aeroservoelastic Systems Using High-Order Iterative Technique System ID Should be review ed w ith 49397M olin Technion 3 3 2 1 0 0 0 0 0 4.7 13748229 Nonlinear Structural Dynamics Characterization by Decomposing Time Signals Using Hilbert-Huang Transform System ID Pai H u U niversity of M issouri-C olum bia 3 3 1 2 0 0 0 0 0 4.3 13849397 Unified Procedure for Structural and Parameteric Identification of Nonlinear Aeroelastic and Aeroservoelastic Systems System ID Should be review ed w ith 49396M olin Baldelli Technion, ZO N A 3 3 1 2 0 0 0 0 0 4.3 13951022 Application of the Random Decrement Technique to a Nonlinear Dynamic System System ID Shiryayev Slater Wright State University 3 3 1 2 0 0 0 0 0 4.3 14048352 Estimates of FRFs from Output-Only Data of a Space Mission Payload Component System ID C rem a C oppotelli U niversit̀a degli Studi di R om a “La Sapienza”3 3 0 3 0 0 0 0 0 4.0 14149560 Statistical Analysis Tools for Detection of Non-Linearity in Aeroelastic Phenomena System ID Aeroelasticity-nonlinear Popescu Wong Lee U niv Alberta, C anada 3 3 1 1 1 0 0 0 0 4.0 14249671 Modeling and Parameter Estimation of Spacecraft Fuel Slosh Using Pendulum Analogs System ID Schlee Gangadharan Sudermann Embry-Riddle, NASA Kennedy, Hubert Aeronautics3 3 0 3 0 0 0 0 0 4.0 14348745 Advanced System Interrogation Based on Active Bifurcation Morphing System ID Yin Epureanu U niv M ichigan 3 3 0 2 1 0 0 0 0 3.7 14450961 Comparison of Inverse Structural Filter (ISF) and Sum of Weighted Accelerations (SWAT) Time Domain Force Identification Methods System ID Allen Carne Sandia 4 2 0 1 1 0 0 0 0 3.5 14551028 Effects of Sensor Placement on Identification Using the Minimum Model Error Algorithm System ID Shiryayev Slater Wright State University 3 2 0 1 1 0 0 0 0 3.5 14648411 Non-Linear System Identification of Theoretical and Experimental Data for Mechanical Systems System ID Vio D im itriadis Shi The U niversity of M anchester 3 3 0 2 0 1 0 0 0 3.0 14750966 A Reduced-Order Model Approach for Turbomachinery Linear Aeroelastic Analysis Turbomachinery Reduced order modelingMunteanu Rajadas Chattopadhyay Arizona State 3 3 1 1 1 0 0 0 0 4.0 14851079 Experimental Monte Carlo Mistuning Assessment of Bladed Disk Vibration Using Forcing Variations Turbomachinery Li Pierre Ceccio Univ Michigan 3 3 2 1 0 0 0 0 0 4.7 14948771 Modeling Cylinder Flow Vortex Shedding with Enforced Motion Using a Harmonic Balance Approach Turbomachinery Spiker Thom as D ow ell D uke 3 3 1 2 0 0 0 0 0 4.3 15048596 A Resonant Synchronous Vibration Based Approach for Rotor Imbalance Detection Turbomachinery Luo R odriguez C orbly G E, N ASA G lenn 3 3 0 3 0 0 0 0 0 4.0 15150916 Aeroelastic Analysis of an Isolated Airfoil and Turbomachinery Blades under a Non-uniform Free Stream Flow Turbomachinery Cho Shin Kim Seoul National, Boeing 3 3 0 0 3 0 0 0 0 3.0 15250884 Hardware Tuning for Dynamic Performance through Isoperformance Tuning Uncertainty analysis and modeling Masterson Miller MIT 3 3 0 3 0 0 0 0 0 4.0 15348238 Robust Flutter Analysis Considering Modeshape Variations U ncertainty analysis and m odelingflutter H einze Borglund Kungliga Tekniska H ögskolan (KTH )3 3 0 2 1 0 0 0 0 3.7 15448722 Uncertainty Propagation and Substructure Synthesis Using LFTs U ncertainty analysis and m odelingStructural dynam ics C arter Babu_k Lane G eneral D ynam ics, AFR L Kirtland3 2 0 1 1 0 0 0 0 3.5 15550967 Girsanov Linearization of Stochastically Driven Nonlinear Oscillators Uncertainty analysis and modeling Saha Roy Indian Institute of Science, Bangalore3 2 0 0 2 0 0 0 0 3.0 156

Selection ProcessSelection Process

Impose:Impose:–– cut-off for 82% acceptance cut-off for 82% acceptance andand–– better than or better than or AvgAvg

Last picks (all 3.0 average) based on topicLast picks (all 3.0 average) based on topicthat might accommodate them in sessionthat might accommodate them in session

Categorized Abstracts into Session TopicsCategorized Abstracts into Session Topics

Good > 3.50Avg 3.0 - 3.49Bad < 3.00

1212

Technical Session Technical Session –– Structural Dynamics Structural Dynamics

Max most of the week and lightened up on Th PM

Sessions AM PM AM PM AM PM AM PM TOTAL

Regular 2 4 4 3 2 3 3 3 24

Special 1 1 1 3

Total 3 4 4 4 3 3 3 3 27

Monday Tueday Wednesday Thursday

Papers AM PM AM PM AM PM AM PM TOTAL

Regular 12 27 28 16 12 20 20 13 148

Special 7 5 panel 12

TOTAL 19 27 28 21 12 20 20 13 160

Max Alloc. 21 28 28 24 18 21 21 18 179

Monday Tueday Wednesday Thursday

1313

Technical Session Technical Session –– Structural Dynamics Structural Dynamics

Sessions# of papers

# of student papers AM PM AM PM AM PM AM PM

Acoustic load 5 0 xActive control 7 0 x

Aeroelastic design 7 0 x

Aeroelasticity 7 2 xAeroservoelasticity 6 0 xBeams 7 0 xComputational Aeroelasticity 7 0 xComputational Structural Dynamics 6 1 xAdvances and Trends in Computational Structural Dynamics--Part II (panel) 0 0 xAdvances and Trends in Computational Structural Dynamics--Part I 5 0 xDamping 5 0 xMAV Structural Analysis and Multibody Dynamics 6 0 xExperimental Aeroelasticity 7 0 xExperimental Structural Dynamics 5 1 xAeroelasticity of HALE Aircraft 7 1 xImpact Load 7 0 xLimit Cycle Oscillations 7 0 xParticle Damping 7 0 xPlates and Shells 7 0 xReduced-order Modeling 6 0 xRotary Wing and Rotorcraft Applications 7 0 xSpacecraft loads and dynamics 6 0 xSystem ID I 7 0 xSystem ID II 6 0 xTurbomachinery 5 0 xUncertainty Analysis 4 0 xWave Propagation 4 0 x

160 3 4 4 4 3 3 3 3

Mon Tue Wed Thu

1414

SummarySummary

Great increase in abstract submittals this yearGreat increase in abstract submittals this year Total # of abstracts: 201Total # of abstracts: 201

–– Abstracts accepted: 160Abstracts accepted: 160–– Abstracts rejected: 33Abstracts rejected: 33–– Abstracts transferred: 8Abstracts transferred: 8

Total reviews performed: 560 (98%)Total reviews performed: 560 (98%) Acceptance Rate: 80% of 201Acceptance Rate: 80% of 201 Total sessions: 27 (up from 21 last year)Total sessions: 27 (up from 21 last year)

–– Regular sessions: 24Regular sessions: 24–– Special sessions: 3 (including 1 Panel session)Special sessions: 3 (including 1 Panel session)

My sincere thanks goes to all of you who reviewed theMy sincere thanks goes to all of you who reviewed theabstracts, and did it in a timely manner! I could not have doneabstracts, and did it in a timely manner! I could not have done

without you!without you!

1515

Next StepsNext Steps

Ordering papers within SessionsOrdering papers within Sessions–– Build sessions in CASBuild sessions in CAS–– Check for conflict within SD SessionsCheck for conflict within SD Sessions–– Check for conflict within all co-located conferencesCheck for conflict within all co-located conferences

Chair/co-chair assignments (Chair/co-chair assignments (I will be e-mailing each oneI will be e-mailing each oneof you to confirm your presence at the Conference so toof you to confirm your presence at the Conference so toparticipate in chairing/co-chairing a sessionparticipate in chairing/co-chairing a session))

Send rejection letters (end of November)Send rejection letters (end of November)

1616

Summary SDMSummary SDM’’06 Planned Papers06 Planned Papers

1717

Education SubcommitteeEducation Subcommittee

Current membersCurrent members–– Yehia El-Aini, Chad Hebert (Chair), William Hughes, TeresaYehia El-Aini, Chad Hebert (Chair), William Hughes, Teresa

Kinney, Kirit Patel, Ted Rose, Joseph Slater, Stephanie Wilson,Kinney, Kirit Patel, Ted Rose, Joseph Slater, Stephanie Wilson,Dan WorthDan Worth

Short CoursesShort Courses–– AeroelasticityAeroelasticity–– Aircraft Design LoadsAircraft Design Loads–– Basic Dynamics Basic Dynamics –– in planning phase in planning phase–– Dynamic Testing Dynamic Testing –– in planning phase in planning phase

Outreach Project DemoOutreach Project Demo

1818

Outreach ProjectOutreach Project

Outreach Project StatusOutreach Project Status–– Pursuing additional funding from NASAPursuing additional funding from NASA–– Need text for video clipsNeed text for video clips–– Media Fusion has a bit of work leftMedia Fusion has a bit of work left

ExperimentsExperiments NarrationNarration ““ExtrasExtras”” PolishPolish

–– Target completion is SDM 2006Target completion is SDM 2006

1919

Outreach ProjectOutreach Project

KiritKirit Patel PatelRay Ray GordnierGordnier

Simulated upperSimulated upperatmospheric, hypersonicatmospheric, hypersonicflightflight

Hyper-XHyper-X

John RogersJohn RogersInderjitInderjit Chopra Chopra

High altitude, supersonicHigh altitude, supersonicflightflight

SR-71 BlackbirdSR-71 Blackbird

FirdausFirdaus UdwadiaUdwadiaDon KunzDon Kunz

Describe buffeting andDescribe buffeting andshock wavesshock waves

Transonic FlightTransonic FlightBell X-1Bell X-1

Joe SlaterJoe SlaterEric AustinEric Austin

How does structuralHow does structuraldynamics help us todynamics help us to““move faster?move faster?”” Tie to Tie tosubsonic, transonic,subsonic, transonic,supersonic andsupersonic andhypersonic flight.hypersonic flight.

--Moving FasterMoving Faster

AuthorsAuthorsTextTextVideoVideoFrameFrame

Maybe should have sub-, trans- and super-sonic instead of trans-, super- andhyper-sonic?

2020

Outreach ProjectOutreach Project

Dexter JohnsonDexter JohnsonTed NyeTed Nye

Describe flexibility ofDescribe flexibility oflarge, lightweight spacelarge, lightweight spacestructures such as ISSstructures such as ISSand solar sailsand solar sails

Simulated MissionSimulated MissionSolar SailSolar Sail

Bruce WillisBruce WillisRameshRamesh MallaMalla

Describe orbital forces,Describe orbital forces,landing loadslanding loads

Simulated missionSimulated missionhighlightshighlights

Moon LandingMoon Landing

Andy Brown (haveAndy Brown (havematerial)material)El-El-AiniAini YehiaYehia

Describe thrustDescribe thrusttransients, acousticstransients, acousticsand vibrationand vibration

LaunchLaunchRedstone RocketRedstone Rocket

Frank Frank PaiPaiHyoungHyoung-Man Kim-Man Kim

How does structuralHow does structuraldynamics help us todynamics help us to““travel farther?travel farther?”” Tie to Tie tolaunch vehicles andlaunch vehicles andlight-weight light-weight spacecaftspacecaft..

--Traveling FartherTraveling Farther

AuthorsAuthorsTextTextVideoVideoFrameFrame

2121

Outreach ProjectOutreach Project

Y.C. Y.C. YiuYiuStephanie WilsonStephanie Wilson

Describe forces onDescribe forces onsatellite vehiclessatellite vehicles

Simulated spacecraftSimulated spacecraftand ISSand ISS

Satellite VehiclesSatellite Vehicles

Rob Rob McAmisMcAmisPaul TaylorPaul Taylor

Describe forces fromDescribe forces frommaneuvers and frommaneuvers and fromwind featureswind features

Flight maneuversFlight maneuversHigh-altitude planesHigh-altitude planes

John John KosmatkaKosmatkaWilliam William WelschWelsch

Describe dynamic Describe dynamic vsvsstatic loadingstatic loading

Early flight attempts (notEarly flight attempts (notall Wright)all Wright)

Wright Plane (Change toWright Plane (Change toEarly Flight?)Early Flight?)

Rick LindRick LindFred Fred NitzscheNitzscheConorConor Johnson Johnson

How does structuralHow does structuraldynamics help us todynamics help us to““reach higher?reach higher?”” Tie to Tie toaircraft, high altitudeaircraft, high altitudeplanes, satellites.planes, satellites.

--Reaching HigherReaching Higher

AuthorsAuthorsTextTextVideoVideoFrameFrame

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Liaison SubcommitteeLiaison Subcommittee Current membersCurrent members

–– Carlos Carlos CesnikCesnik, Ray , Ray GordnierGordnier, , KiritKiritPatel, Patel, SuryaSurya SurampudiSurampudi, Bruce Willis, Bruce Willis(Chair), Dan Worth(Chair), Dan Worth

Report by Bruce WillisReport by Bruce Willis

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Publications SubcommitteePublications Subcommittee

Current membersCurrent members–– Eric Austin, Frank Eric Austin, Frank PaiPai , Suresh , Suresh ShrivastavaShrivastava (Chair), (Chair),

IsamIsam YunisYunis

NewsletterNewsletter–– Suresh Suresh ShrivastavaShrivastava volunteered to be the editor volunteered to be the editor–– Draft in workDraft in work–– Consider submitting an articleConsider submitting an article

InformationalInformational EditorialEditorial

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Publications SubcommitteePublications Subcommittee

Year-in-Review articleYear-in-Review article–– Suresh Suresh ShrivastavaShrivastava edited the article edited the article –– THANK THANK

YOU!YOU!–– 6 contributors - THANK YOU!6 contributors - THANK YOU!–– 625 words (575 required) plus one photo625 words (575 required) plus one photo

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Secretariat SubcommitteeSecretariat Subcommittee

Current membersCurrent members–– Andy Brown (Secretariat)Andy Brown (Secretariat)

Roster updatesRoster updates Technical Expert DatabaseTechnical Expert Database

–– Communication mechanism to distribute timelyCommunication mechanism to distribute timelyinformation relating to aerospace public policy issuesinformation relating to aerospace public policy issuesand strategiesand strategies

–– SDTC to support initiative by providing names for areasSDTC to support initiative by providing names for areasof expertiseof expertise

–– Secretariat will maintain spreadsheetSecretariat will maintain spreadsheet

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Standards Working GroupStandards Working Group

Current MembersCurrent Members–– Andy Brown, Andy Brown, HyoungHyoung-Man Kim, Teresa Kinney (Chair),-Man Kim, Teresa Kinney (Chair),

IsamIsam YunisYunis

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Technology Assessment and TransferTechnology Assessment and TransferSubcommitteeSubcommittee

Current membersCurrent members–– Raymond Gordnier, Raymond Gordnier, ConorConor Johnson, Dexter Johnson , Johnson, Dexter Johnson , HyoungHyoung-Man-Man

Kim (Chair), Rob McAmis, Ted Nye, John Rogers, and StephanieKim (Chair), Rob McAmis, Ted Nye, John Rogers, and StephanieWilsonWilson

Current status/planCurrent status/plan–– Updating the structure of the structural dynamics technologiesUpdating the structure of the structural dynamics technologies

reference websitereference website Most of the government agencies and large companies do no longerMost of the government agencies and large companies do no longer

put their technical related web pages in the world wide web (www)put their technical related web pages in the world wide web (www) Many of the company web pages give too much commercial flavorsMany of the company web pages give too much commercial flavors

–– Requested to SDTC members for their input, but did not receiveRequested to SDTC members for their input, but did not receivemuch inputmuch input Need help!Need help!

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Technology Assessment and TransferTechnology Assessment and TransferSubcommitteeSubcommittee

Structural dynamics technologies referenceStructural dynamics technologies referencewebsite inputwebsite input–– Category No. (e.g. 2.3.1, etc.)Category No. (e.g. 2.3.1, etc.)–– Web AddressWeb Address–– Appropriate Website Title (sometimes, the defaultAppropriate Website Title (sometimes, the default

website title does not reflect the contents accurately)website title does not reflect the contents accurately)–– Short Description (about 20 words or less)Short Description (about 20 words or less)

Before sending the input, need to check theBefore sending the input, need to check thewebsites at home to see if people can get to themwebsites at home to see if people can get to themfrom outside of your organizationfrom outside of your organization

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Structural Dynamics Technologies ReferenceStructural Dynamics Technologies ReferenceWebsite CategoriesWebsite Categories

1.0 Foundation Technologies1.0 Foundation Technologies–– 1.1 Analysis1.1 Analysis

1.1.1 Dynamics Simulation1.1.1 Dynamics Simulation 1.1.2 Finite-Element Modeling1.1.2 Finite-Element Modeling 1.1.3 Reduced-Order Modeling1.1.3 Reduced-Order Modeling 1.1.4 Component Mode Synthesis1.1.4 Component Mode Synthesis 1.1.5 Fluid-Structure and 1.1.5 Fluid-Structure and AeroelasticAeroelastic

AnalysisAnalysis 1.1.6 Statistical Energy Analysis1.1.6 Statistical Energy Analysis 1.1.7 Random Vibrations1.1.7 Random Vibrations 1.1.8 Shock and Transient Analysis1.1.8 Shock and Transient Analysis 1.1.9 Analytical Services1.1.9 Analytical Services

–– 1.2 Design1.2 Design 1.2.1 Computer-Aided Design1.2.1 Computer-Aided Design 1.2.2 Design Services1.2.2 Design Services

–– 1.3 Vibration Damping and Isolation1.3 Vibration Damping and Isolation 1.3.1 Vibration Controls1.3.1 Vibration Controls 1.3.2 Isolation Mounts1.3.2 Isolation Mounts 1.3.3 Damping Materials1.3.3 Damping Materials 1.3.4 Damping Design1.3.4 Damping Design

–– 1.4 Instrumentation and Testing1.4 Instrumentation and Testing 1.4.1 Sensors1.4.1 Sensors 1.4.2 Data Acquisition and Analysis1.4.2 Data Acquisition and Analysis 1.4.3 System Identification1.4.3 System Identification 1.4.4 Test Data Analysis1.4.4 Test Data Analysis 1.4.5 Testing Facilities and Services1.4.5 Testing Facilities and Services

2.0 Applied Technologies2.0 Applied Technologies–– 2.1 Acoustic and Noise Control2.1 Acoustic and Noise Control–– 2.2 Active Vibration Control2.2 Active Vibration Control

2.2.1 Government Laboratory2.2.1 Government LaboratoryOrganizationsOrganizations

2.2.2 Government-Industry Programs2.2.2 Government-Industry Programs 2.2.3 University Activities, Laboratories,2.2.3 University Activities, Laboratories,

and Programsand Programs–– 2.3 2.3 AeroelasticitiyAeroelasticitiy, Fluid- and Control-, Fluid- and Control-

Structure InteractionStructure Interaction 2.3.1 2.3.1 AeroelasticityAeroelasticity 2.3.2 Fluid-Structure Interactions2.3.2 Fluid-Structure Interactions 2.3.3 Control-Structure Interactions2.3.3 Control-Structure Interactions

((ServoelasticityServoelasticity))

3.0 Other Technology Resources3.0 Other Technology Resources–– 3.1 Databases3.1 Databases–– 3.2 Events and Exhibits3.2 Events and Exhibits–– 3.3 Technology Transfer Offices and3.3 Technology Transfer Offices and

OrganizationsOrganizations 3.3.1 National Technology Transfer3.3.1 National Technology Transfer

ResourcesResources 3.3.2 Government Laboratory Technology3.3.2 Government Laboratory Technology

Transfer OfficesTransfer Offices 3.3.3 Technical Information Resources;3.3.3 Technical Information Resources;

Technology Assessment and CooperativeTechnology Assessment and CooperativePrograms Offices (Europe)Programs Offices (Europe)

–– 3.4 Journals3.4 Journals–– 3.5 Books3.5 Books

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Website SubcommitteeWebsite Subcommittee

Current membersCurrent members–– Steve Lane, Bruce Willis, Dan Worth (Chair)Steve Lane, Bruce Willis, Dan Worth (Chair)

Website needs to be revamped Website needs to be revamped –– BADLY! BADLY!–– Contacted AIAA HQ for helpContacted AIAA HQ for help–– Needs follow-upNeeds follow-up

Harry Harry HimmelblauHimmelblau has offered material to be has offered material to beposted on the website!posted on the website!

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Old BusinessOld Business MembershipMembership

–– Total - 41Total - 41 Industry - 14Industry - 14 Academia - 13Academia - 13 Government - 14Government - 14 Associate - 2Associate - 2 International International –– 2 2

Please solicit young membership Please solicit young membership –– sponsor an sponsor anAssociate SDTC memberAssociate SDTC member

Nominations for new members are due 1 NovemberNominations for new members are due 1 November–– Forms at Forms at www.aiaa.orgwww.aiaa.org, under , under ““inside AIAAinside AIAA”” then then ““TechnicalTechnical

CommitteesCommittees””

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Old BusinessOld Business STS-121 MementoSTS-121 Memento

–– Stephanie Wilson offered to fly a mementoStephanie Wilson offered to fly a mementofor the SDTCfor the SDTC

–– American FlagAmerican Flag–– SDTC will frame post-flightSDTC will frame post-flight–– Chair may display plaqueChair may display plaque

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New BusinessNew Business Contributions to SocietyContributions to Society

–– Identify a contribution or benefit to society fromIdentify a contribution or benefit to society fromyour aerospace technologyyour aerospace technology

–– Categorize as meeting one or more of theCategorize as meeting one or more of thefollowing needs:following needs: SafetySafety SecuritySecurity PrestigePrestige KnowledgeKnowledge Helping othersHelping others

–– Suggestions for SDTC topicsSuggestions for SDTC topics

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Contributions to Society Contributions to Society ––Template for InputTemplate for Input

Request new inputs use this templateRequest new inputs use this template

Name/Title of contribution TCTC Rep name Phone email1-2 line summary

1-2 paragraph explanation With as much specifics as possibleWhat is the technology/contributionWho developed (individual/team)Where developedWhen developedWhy developed - original intentHow is it used in aerospace industryHow is it used in societyExamples of specific usesImpact if technology removed/not availableSelect one need the contribution addresses from the list below

Safety Security Prestige Knowledge Helping Others

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Contributions to Society Contributions to Society ––Questions/ThoughtsQuestions/Thoughts

How deep? As deep as necessary to explain the benefit orHow deep? As deep as necessary to explain the benefit orcontribution to societycontribution to societyTimeframe for submittal: Next round will be presented at TAC inTimeframe for submittal: Next round will be presented at TAC inJanuary 2006January 2006TC Contribution TC Contribution vsvs technology contribution: Looking for both technology contribution: Looking for bothHistory History vsvs current: Looking for both; modern contributions help our current: Looking for both; modern contributions help ourpublic policy efforts more readily, and we can recognize thepublic policy efforts more readily, and we can recognize thecontributors as wellcontributors as wellHistorical perspectives can be useful for History TC programsHistorical perspectives can be useful for History TC programsContributions can be international in scope.Contributions can be international in scope.

Contact info:[email protected]

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AdjournmentAdjournment

Thank you to our host - Joe SlaterThank you to our host - Joe Slater Thank you for supporting Thank you for supporting –– in person or via in person or via

telecontelecon Topics for spring meetingTopics for spring meeting

–– Election for chair and vice-chairElection for chair and vice-chair

Liaison Report to Structural Dynamics Technical Committee Oct. 19, 2005 Fall Meeting

For the Adaptive Structures TC, there is no much to report since the SDM. The most interesting point is that the book project: "AIAA Progress in Aeronautics and Astronautics Volume: Adaptive Materials and Structures" (equivalent to our quasi-eternal video/DVD project) is collecting abstracts from the participants who will write chapters. The complete draft is scheduled to be sent to AIAA by the time of the SDM'06. Nothing from Flight Test, Materials, Structures, Applied Aerodynamics, or Ground Test TCs.