TY - GEN
T1 - Design, Analyses, and Flutter Testing of the Active Aeroelastic Aircraft Testbed (A3TB) Platform
AU - Joels, Tsoof
AU - Yechiely, Noam
AU - Gabay, Amit
AU - Griehanovsky, Jenya
AU - Winter, Matan
AU - Moatgonieiy, Oren
AU - Boulahjar, Saber
AU - Glamw, Yishay
AU - Biberstein, Guy Gordon
AU - Edery-Azulay, Lucy
AU - Raveh, Daniella E.
N1 - Publisher Copyright: © 2022 IACAS 2022 - 61st Israel Annual Conference on Aerospace Science. All rights reserved.
PY - 2022
Y1 - 2022
N2 - The paper presents the design, analyses, and flutter flight testing of the Active Aeroelastic Aircraft Testbed (A 3 T B), a 3D-printed aeroelastic demonstrator vehicle. The A 3 T B is a Hying-wing configuration designed as a modular experimental research platform, to demonstrate static and dynamic aeroelastic shape control that targets performance and stability goals. The aircraft design is accompanied with detailed discipliniiry models and analyses of the aerodynamics, structures, and aeroelastic response, which weie verified in giound and flight tests. The papei- presents the A 3 T B design, models, aerodynamic, dynamic, and aeroelastic characteristics, and data analysis of a flutter flight test. The A 3 T B, with its verihed detailed models, is available tor future experimental studies of flutter suppression and aeroelastic twitiol.
AB - The paper presents the design, analyses, and flutter flight testing of the Active Aeroelastic Aircraft Testbed (A 3 T B), a 3D-printed aeroelastic demonstrator vehicle. The A 3 T B is a Hying-wing configuration designed as a modular experimental research platform, to demonstrate static and dynamic aeroelastic shape control that targets performance and stability goals. The aircraft design is accompanied with detailed discipliniiry models and analyses of the aerodynamics, structures, and aeroelastic response, which weie verified in giound and flight tests. The papei- presents the A 3 T B design, models, aerodynamic, dynamic, and aeroelastic characteristics, and data analysis of a flutter flight test. The A 3 T B, with its verihed detailed models, is available tor future experimental studies of flutter suppression and aeroelastic twitiol.
UR - http://www.scopus.com/inward/record.url?scp=85143257219&partnerID=8YFLogxK
M3 - منشور من مؤتمر
T3 - IACAS 2022 - 61st Israel Annual Conference on Aerospace Science
BT - IACAS 2022 - 61st Israel Annual Conference on Aerospace Science
T2 - 61st Israel Annual Conference on Aerospace Science, IACAS 2022
Y2 - 9 March 2022 through 10 March 2022
ER -