Large-scale wind-tunnel tests of a deflected slipstream STOL model with wings of various aspect ratios / V. Robert Page, Stanley O. Dickinson, Wallace H. Deckert.
|Main Author:||Page, V. Robert.|
|Other Authors:||Dickinson, Stanley O. , Deckert, W. H.|
Washington, D.C. : National Aeronautics and Space Administration ; 1968.
Short take-off and landing aircraft
> Design and construction.
Short take-off and landing aircraft > Longitudinal stability.
Propeller-driven aircraft > Testing.
Wind tunnel testing.
53 p. :
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