AIAA-2004-4969 Experimental Aerodynamic Study of UAV Wind Tunnel Model for Low Reynolds Number
22nd, AIAA applied aerodynamics conference ; 2004 ; Providence, RI
AIAA applied aerodynamics conference ; 516-522
2004-01-01
7 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
DataCite | 1940
Pulsed Plasma Thruster for Multi-Axis CubeSat Attitude Control Applications (AIAA 2018-4969)
British Library Conference Proceedings | 2018
|AIAA-2004-6812 Force Balance Measurement Sensor in Wind Tunnel Aerodynamic Testing Environments
British Library Conference Proceedings | 2004
|