Wind-tunnel tests of rectangular Clark Y wing made with N A C A spinning balance; all six components of aerodynamic force and moment were measured throughout range of angles of attack and angles of sideslip, likely to be attained by spinning airplane; application of data from spinning balance to estimation of angle of sideslip necessary for spinning equilibrium at any angle of attack. (Price 10¢)
Spinning characteristics of wings. I -- Rectangular Clark Y monoplane wing
Nat Advisory Committee Aeronautics -- Report
1935
20 pages
Bibliography
Report
Englisch
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Engineering Index Backfile | 1937
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