Span loadings and aerodynamic characteristics for a series of tip and trailing-edge controls on a 60° delta wing at Mach numbers of 1.61 and 2.01 /
by K. R. Czarnecki and Douglas R. Lord.

Description

Main Author: Czarnecki, K. R.
Related Names: Lord, Douglas R.
Langley Research Center.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration, 1959.
Subjects: Trailing edges (Aerodynamics)
Mach number.
Airplanes > Airplanes / Wings, Triangular > Airplanes / Wings, Triangular / Testing.
Aerodynamic load.
Note: "September 1959."
Cover title.
Full text also available online. Address as of 11/15/2010:
Physical Description: 118 p. : ill. ; 26 cm.
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Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign