Rotary balance data for a single-engine trainer design for an angle-of-attack range of 8 degree to 90 degree
Rotary balance data for a single-engine trainer design for an angle-of-attack range of 8 degree to 90 degree
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- Washington, D.C. National Aeronautics and Space Administration 1980
- 324 p.
- NASA CR 3099 : 1979 .
General aviation, Spinning, Rotary balance, High angle-of-attack wind tunnel
LNASA CR 3099 : 1979
General aviation, Spinning, Rotary balance, High angle-of-attack wind tunnel
LNASA CR 3099 : 1979