Tests are part of general investigation being made in NACA free spinning tunnel to determine effect of systematic changes in wing and tail arrangement upon steady spinning and recovery characteristics of conventional low wing monoplane for various loading conditions.
Free-spinning wind-tunnel tests of low-wing monoplane with systematic changes in wings and tails, II mass distributed along fuselage, III. mass distributed along wings
Nat Advisory Committee Aeronautics -- Tech Note
1937
11 pages
17 Supp sheets, Bibliography
Report
Englisch
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