Wind-tunnel investigation of the aerodynamic characteristics of a model representative of a supersonic fighter-class airplane with an external-flow jet-augmented flap in low-speed flight / by William A. Newsom, Jr.
|Main Author:||Newsom, William A.|
Washington, [D.C.] : National Aeronautics and Space Administration, 1959.
Externally blown flaps.
Wind tunnel models.
Wind tunnel tests.
Augmentation flaps (control surfaces)
Title from cover.
"Langley Research Center, Langley Field, Va."
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 11/17/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068069_1989068069.pdf.
"NASA TN D-50."
84 p. :
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