Apparatus and techniques were developed for measuring in a low-speed wind tunnel the static and dynamic (rotary balance) aerodynamic data pertinent to spin behavior of a general aviation aircraft. The main results were: (1) collection of static force and moment data for several airplane configurations at angles of attack from 0 to 90 degrees and angles of sideslip from 0 to 40 degrees; and (2) difficulties, shortcomings, and unsuitability of some aspects of the rotary balance mount as constructed were discovered and identified for avoidance in a new design for a mount.
Development of capabilities for stall/spin research
1976-06-20
Report
No indication
English
Development of Capabilities for Stall/Spin Research
NTIS | 1976
|Stall/Spin Research Status Report
SAE Technical Papers | 1974
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NTRS | 1974
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British Library Conference Proceedings | 2014
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