Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing /
by Edward C. Polhamus and Kenneth P. Spreemann.

Description

Main Author: Polhamus, Edward C.
Related Names: Spreemann, Kenneth P.
United States. National Aeronautics and Space Administration.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration : [1961]
Subjects: Stability and control.
Aircraft.
Note: Cover title.
"May 1961."
Aircraft; Stability and control.
Physical Description: 32 p. : ill. ; 26 cm.
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Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign