Spin-Tunnel Investigation of a 1/28-Scale Model of a Subsonic Attack Airplane
Description:
"An investigation has been made of a 1/28-scale model of the Grumman A-6A airplane in the Langley spin tunnel. The erect spin and recovery characteristics of the model were determined for the flight design gross weight loading and for a loading with full internal fuel and empty external wing fuel tanks. The effects of extending slats and deflecting flaps were investigated" (p. 1).
Date:
July 1964
Creator:
Lee, Henry A. & Healy, Frederick M.
Item Type:
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