Force Balance Measurement Sensor in Wind Tunnel Aerodynamic Testing Environments
USAF Developmental Test and Evaluation Summit
01.01.2004
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
AIAA-2004-6812 Force Balance Measurement Sensor in Wind Tunnel Aerodynamic Testing Environments
British Library Conference Proceedings | 2004
|New aerodynamic balance for the MIRA full-scale wind tunnel
Kraftfahrwesen | 1987
|Kraftfahrwesen | 1983
|Hotshot Wind Tunnel Force Measurement
IEEE | 1965
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