The present paper discusses the NASA Langley Research Center stall/spin research program to improve the design and the evaluation techniques relative to stall/spin characteristics of general-aviation aircraft. The program encompasses model wind-tunnel tests, spin-tunnel and radio-control model tests, and full-scale airplane spin tests. Initial spin-tunnel results on models with several tail designs representative of light airplanes and several testing techniques are discussed.
Stall/spin studies relating to light general-aviation aircraft.
Business Aircraft Meeting ; 1973 ; Wichita, KS
1973-04-01
Conference paper
No indication
English
STALL/SPIN STUDIES RELATING TO LIGHT GENERAL-AVIATION AIRCRAFT
SAE Technical Papers | 1973
|A Stall/Spin Prevention Device for General-Aviation Aircraft
SAE Technical Papers | 1973
|