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Southwest Research Institute® (SwRI®) structural engineering spe- cialists have a combined total of more than 150 years of experience in anal- ysis of structures under various load conditions. SwRI employs the latest technology in computational simula- tion to provide clients with real-time data formatted for accurate analysis and verification of finite element analysis. SwRI’s analytical capabilities are supplemented by testing of struc- tures to substantiate the models. Capabilities SwRI has the capability to perform all levels of structural analysis, from individual components to complete assemblies. Development of finite ele- ment models from geometric data or modification of existing models for component improvement or repair is included in these capabilities. The staff has performed stress analysis ser- vices for commercial and government clients in many areas of aircraft struc- tures, including wing, empennage, fuselage, landing gear, and whole air- craft modeling and simulation. Experience n Expand/review/refine existing finite element models (FEM) n Idealization of wing, fuselage and specialized structural models n Experimental validation of FEM n New finite models from geometric models (CAD) or historical loft data Aircraft Structural Analysis D015725 KEYWORDS Structural Analysis Finite Element Modeling (FEM) Finite Element Analysis (FEA) Classical Analysis Bonded Composite Structure Structural Repair and Modification Damage Tolerance Analysis (DTA) Durability and Damage Tolerance Analysis (DADTA) Structural Life Enhancement Simulation Idealization Validation Southwest Research Institute ® Finite element model (FEM) of aircraft forward fuselage Detailed modeling for repair development and support for damage tolerance analysis Typical FEM stress contours on deformed wing n FEM usage; development of component repair scheme n Models for composite repair of metallic structures n Modeling of composite materials n Analysis of repair and maintenance actions n Engineering support at customer location D015726 D015727
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Aircraft Structural Analysis - Southwest Research · PDF fileTitle: Aircraft Structural Analysis Author: Kenneth E. Griffin Subject: Aircraft Structural Analysis Keywords: Structural

Jan 30, 2018

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Page 1: Aircraft Structural Analysis - Southwest Research · PDF fileTitle: Aircraft Structural Analysis Author: Kenneth E. Griffin Subject: Aircraft Structural Analysis Keywords: Structural

Southwest Research Institute® (SwRI®) structural engineering spe-cialists have a combined total of more than 150 years of experience in anal-ysis of structures under various load conditions. SwRI employs the latest technology in computational simula-tion to provide clients with real-time data formatted for accurate analysis and verification of finite element analysis. SwRI’s analytical capabilities are supplemented by testing of struc-tures to substantiate the models.

CapabilitiesSwRI has the capability to perform all levels of structural analysis, from individual components to complete assemblies. Development of finite ele-ment models from geometric data or modification of existing models for component improvement or repair is included in these capabilities. The staff has performed stress analysis ser-vices for commercial and government clients in many areas of aircraft struc-tures, including wing, empennage, fuselage, landing gear, and whole air-craft modeling and simulation.

Experience n Expand/review/refine existing finite element models (FEM) n Idealization of wing, fuselage and specialized structural models

n Experimental validation of FEM

n New finite models from geometric models (CAD) or historical loft data

Aircraft Structural Analysis

D01

5725

KEYWORDS

Structural Analysis

Finite Element Modeling (FEM)

Finite Element Analysis (FEA)

Classical Analysis

Bonded Composite Structure

Structural Repair and Modification

Damage Tolerance Analysis (DTA)

Durability and Damage Tolerance Analysis (DADTA)

Structural Life Enhancement

Simulation

Idealization

Validation

SouthwestResearchInstitute®

Finite element model (FEM) of aircraft forward fuselage

Detailed modeling for repair development and support for damage tolerance analysis

Typical FEM stress contours on deformed wing

n FEM usage; development of component repair scheme

n Models for composite repair of metallic structures

n Modeling of composite materials

n Analysis of repair and maintenance actions

n Engineering support at customer locationD

0157

26D

0157

27

Page 2: Aircraft Structural Analysis - Southwest Research · PDF fileTitle: Aircraft Structural Analysis Author: Kenneth E. Griffin Subject: Aircraft Structural Analysis Keywords: Structural

Benefiting government, industry and the public

through innovative science and technology

Kenneth E. Griffin, Ph.D., Manager David H. Wieland, Principal EngineerAerospace Structures Aerospace Structures(210) 522-6873 (210) [email protected] [email protected]

Department of Structural EngineeringMechanical Engineering DivisionSouthwest Research Institute6220 Culebra Road (78238-5166)P.O. Drawer 28510 (78228-0510)San Antonio, Texas

www.swri.orgwww.aerospacestructures.swri.org

Full aircraft FEM development, verification, validation and analytical application

An Equal Opportunity Employer M/F/D/VCommitted to Diversity in the Workplace

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Analysis Tools

n MSC.NASTRAN®, ANSYS®, ABAQUS® FEM solvers

n StressCheck®

n PATRAN®, FEMAP, Pro/ENGINEER® pre- and post-processors

n Software supported by high-end PC platforms for multiple users simultaneously

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We welcome your inquiries.

For additional information, please contact:

Southwest Research Institute is an independent, nonprofit, applied engineering and physical sciences research and development organi-zation using multidisciplinary approaches to problem solving. The Institute occupies 1,200 acres in San Antonio, Texas, and provides more than 2 million square feet of laboratories, test facilities, work-shops and offices for more than 3,100 employees who perform contract work for industry and government clients.