Full-scale wind-tunnel tests of a low-aspect-ratio, straight-wing airplane with blowing boundary-layer control on leading- and trailing-edge flaps /
by Mark W. Kelly, William H. Tolhurst, Jr., and Ralph L. Maki.

Description

Main Author: Kelly, Mark W.
Related Names: Maki, Ralph L.
Tolhurst, William H.
Ames Research Center.
Language(s): English
Published: Washington, [D.C.] : National Aeronautics and Space Administration, 1959.
Subjects: Longitudinal stability.
Lift.
Lateral control.
Landing speed.
Boundary layer separation.
Wind tunnel tests.
Trailing edge flaps.
Leading edge flaps.
F-104 aircraft.
Boundary layer control.
Blowing.
Note: "NASA TN D-135."
"Ames Research Center, Moffett Field, Calif."
"September 1959."
Title from cover.
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 12/12/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068199_1989068199.pdf.
Physical Description: 24 p. : ill. ; 26 cm.
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