Account of tests made in NACA free spinning tunnel to determine effect of systematic changes in wing and tail arrangements upon steady spinning and recovery characteristics of conventional low wing monoplane model for basic loading conditions.
Free-spinning wind-tunnel tests of low-wing monoplane with systematic changes in wings and tails, I -- Basic loading condition
Nat Advisory Committee Aeronautics -- Tech Notes
1937
13 pages
17 Supp plates, Bibliography
Report
Englisch
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