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Aerodynamics of guided and unguided weapons /
by Frank G. Moore.

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Main Author
Moore, Frank G. (Frankie Gale), 1944-.
Related Names
McKerley, C. William.
Naval Weapons Laboratory (U.S.).
Language(s)
English
Published
Dahlgren, Va. : U.S. Naval Weapons Laboratory, 1973-74.
Dahlgren, Virginia : Naval Weapons Laboratory,
Subjects
Guided missiles > Aerodynamics > Mathematical models > Computer programs.
Projectiles, Aerial > Aerodynamics > Mathematical models > Computer programs.
Summary
Several theoretical and empirical procedures are combined into a single computer program to predict lift, drag, and center of pressure on quite general wing-body geometries. The method is applicable for Mach number zero to three and angle-of-attack zero to about fifteen degrees. Computed results for several configurations compare well with experimental and other analytical results. It costs about five dollars per Mach number to compute the static aerodynamics of a typical wing-body shape on the CDC 6700 computer.
Note
"NWL Technical Report TR-3036 January 1974"--T.p., pt. 2.
"NWL Technical Report TR-3018 December 1973"--T.p., pt. 1.
This work is part of the library's "Parachute History Collection", donated by Sandia National Laboratories through the American Institute of Aeronautics and Astronautics Aerodynamic Deceleration Systems Technical Committee.
Pt. 2 co-authored by C. William McKerley.
Physical Description
2 parts : illustrations, figures ; 28 cm.
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