Stability and control characteristics of a large-scale deflected slipsteam STOL model with a wing of 5.7 aspect ratio / by V. Robert Page and Thomas N. Aiken.
|Main Author:||Page, V. Robert.|
|Other Authors:||Aiken, Thomas N.|
Washington, D.C. : National Aeronautics and Space Administration, 1971.
Stability of airplanes.
Short take-off and landing aircraft.
Airplanes > Wings.
Prepared at Ames Research Center.
v, 62 p. :
|Original Classification Number:||TL500 .T33 71-03798|
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