Low-speed wind-tunnel investigation of blowing boundary-layer control on leading- and trailing-edge flaps of a full-scale, low-aspect-ratio, 42° swept-wing airplane configuration /
by Ralph L. Maki and Demo J. Giulianetti.

Description

Main Author: Maki, Ralph L.
Related Names: Giulianetti, Demo J.
Ames Research Center.
Language(s): English
Published: Washington, [D.C.] : National Aeronautics and Space Administration, 1959.
Subjects: Wind tunnel tests.
Pitching moments.
Lift.
Flow distribution.
Drag.
Aircraft configurations.
Trailing edge flaps.
Swept wings.
Low speed wind tunnels.
Leading edge flaps.
Externally blown flaps.
Boundary layer control.
Note: "NASA TN D-16."
"Ames Research Center, Moffett Field, Calif."
"August 1959."
Cover title.
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 10/23/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068287_1989068287.pdf.
Physical Description: 29 p. : ill. ; 26 cm.
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