Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels /
by M. Leroy Spearman and Gerald V. Foster.

Description

Main Author: Spearman, M. Leroy.
Related Names: Foster, Gerald V.
Langley Research Center.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration, 1961.
Subjects: Short take-off and landing aircraft.
Vertically rising aircraft > Vertically rising aircraft / Aerodynamics.
Stability of airplanes, Lateral.
Stability of airplanes, Longitudinal.
Airplanes > Airplanes / Wings, Triangular.
Airplanes > Airplanes / Wings, Swept-back.
Note: "December 1961."
Cover title.
Full text also available online. Address as of 11/15/2010:
Physical Description: 31 p. : ill. ; 26 cm.
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Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign