Effects of a lower surface jet on the lift-drag ratio of a 45° sweptback wing at a Mach number of 2.01 /
by Emma Jean Landrum.

Description

Main Author: Landrum, Emma Jean.
Related Names: Langley Research Center.
Language(s): English
Published: Washington, [D.C.] : National Aeronautics and Space Administration, 1960.
Subjects: Wind tunnel tests.
Mach number.
Lift.
Flow distribution.
Angular momentum.
Aerodynamic interference.
Under surface blowing
Sweptback wings.
Supersonic flow.
Lift drag ratio.
Jet flow.
Aerodynamic coefficients.
Note: "NASA TN D-183."
"Langley Research Center, Langley Field, Va."
"March 1960."
Title from cover.
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 12/20/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068206_1989068206.pdf.
Physical Description: 40 p. : ill. ; 26 cm.
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Item Link	Original Source
Full view v.183	University of Illinois at Urbana-Champaign