Final results on the development of a precision and automated capability for determining dynamic data for modular aerodynamic configurations (MAC) in free-flight are presented. The system developed includes a modified single engine aircraft with bomb release and various electronic capabilities, a digital telemetry system, a telemetry receiving van with associated receiving and recording elements, and the MAC's with instrumentation devices, soft recovery parachute systems and flight safety equipment. Descriptions are given of drop test of MAC's from the aircraft and of MAC wind tunnel tests. (Author)
Aeromechanics Prediction and Analysis Techniques
1974
48 pages
Report
No indication
English
Aircraft , Bombs , Detonations, Explosion Effects, & Ballistics , Aerodynamic configurations , Free fall missiles , Aerodynamic characteristics , Mathematical prediction , Modular construction , Drop tests , Free flight models , External stores , Release mechanisms , Telemeter systems , Ground stations , Instrumentation , Surface to air , Measurement , Telemetering receivers , Soft landings , Parachutes , Recovery , Data acquisition , Automation , Research planes , Training planes , Bomb racks , Modification , Free flight trajectories , Aviation safety , Flight testing , Wind tunnel tests , Digital systems , Tape recording , Radio signals , L band , Computer applications , Aeromechanics , Cessna 172 aircraft
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