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.
Augmentation flaps (control surfaces)
Wind tunnel tests.
Wind tunnel models.
Externally blown flaps.
"NASA TN D-50."
"Langley Research Center, Langley Field, Va."
Title from cover.
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.
84 p. :
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