Results of an investigation of a dynamic model in the Langley 20-foot free-spinning tunnel are presented. Erect spin and recovery characteristics were determined for a range of mass distributions and center-of-gravity positions. The effects of lateral displacement of the center of gravity, engine rotation, nose strakes, and increased rudder area were investigated.
Free-Spinning-Tunnel Investigation of a 1/17 Scale Model of the Cessna T-37A Airplane
1958
16 pages
Report
Keine Angabe
Englisch
Teardown Evaluation of a 1979 Cessna 402C Model Airplane
NTIS | 2007
|Free-spinning-tunnel tests of model of canard airplane
Engineering Index Backfile | 1943
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