This paper will present the scope of an NASA program aimed at improving the design and evaluation techniques relative to stall/spin characteristics of general-aviation aircraft. The program encompasses analytical studies, full-scale and model wind-tunnel tests, radio-control model, and full-scale flight tests. Initial spin-tunnel results of several tail designs on a representative light airplane will be discussed.
Stall/Spin Research Status Report
Sae Technical Papers
National Business Aircraft Meeting and Engineering Display ; 1974
1974-02-01
Aufsatz (Konferenz)
Englisch
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