Large-scale wind-tunnel tests and evaluation of the low-speed performance of a 35 degree sweptback wing jet transport model equipped with a blowing boundary-layer-control flap and leading edge slat /
by David H. Hicket and Kiyoshi Aoyagi.
Description
- Language(s)
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English
- Published
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Washington, D.C. : National Aeronautics and Space Administration : [1960]
- Note
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Cover title.
"October 1960."
Aerodynamics, aircraft.
- Physical Description
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52 p. :
ill. ;
26 cm.
Viewability
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University of Illinois at Urbana-Champaign
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