Slide 1THE EFFECT OF DOWNSTREAM SUCTION ON THE DELTA WING LEADING-EDGE VORTEX Zhou Ji, Jeff Marchetta, J. Hochstein and J. D. Mo University of Memphis, Memphis, TN 38152,…

AIAA 2001-0124 Application of MEMS Devices to Delta Wing Aircraft: From Concept Development to Transonic Flight Test A.Huang, C. Folk, C. Silva, B. Christensen, Y. Chen,…

AIAA 2001-0124 Application of MEMS Devices to Delta Wing Aircraft: From Concept Development to Transonic Flight Test A.Huang, C. Folk, C. Silva, B. Christensen, Y. Chen,…

INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, VOL. 22,495-5 13 (1 996) A VORTEX LATTICE METHOD FOR HIGH-SPEED PLANING CANHAl LAI AND ARMIN W. TROESCH Department…

JJ70. Book of Abstracts Salamanca, 3rd-4th of September. 2015 Controlling the Flow on Swept Back & Blended Wing Airplane Configurations. I. Wygnanski, The University…

SimSAC Simulating Aircraft Stability and Control Characteristics for use in Conceptual Design —— Specific Targeted Research Project Start: 01 November 2006 Duration:…

Vortex Visualization in Ultra Low Reynolds Number Insect Flight Christopher Koehler, Thomas Wischgoll, Haibo Dong, and Zachary Gaston Fig. 1. Vortex formation, attachment…

Oliver Breitenstein Development of a Flapping Wing Mechanism Semester Project Autonomous Systems Lab (ASL) Swiss Federal Institute of Technology (ETH) Zurich Supervision…

AERODYNAMICS OF WINGS AT LOW REYNOLDS NUMBERS by John McArthur A Qualifying Exam Proposal Presented to the FACULTY OF THE GRADUATE SCHOOL UNIVERSITY OF SOUTHERN CALIFORNIA…