Effects of nose bluntness, fineness ratio, cone angle, and model base on the static aerodynamic characteristics of blunt bodies at Mach numbers of 1.57, 1.80, and 2.16 and angles of attack up to 180 ̊/
David S. Shaw, Dennis E. Fuller, and C. Donald Babb.

Description

Main Author: Shaw, David S.
Related Names: Babb, C. Donald.
Fuller, Dennis E.
Langley Research Center.
United States. National Aeronautics and Space Administration.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration ; 1963.
Subjects: Angle of attack (Aerodynamics)
Blunt bodies > Blunt bodies / Aerodynamics.
Cone > Cone / Aerodynamics.
Noses (Space vehicles) > Noses (Space vehicles) / Aerodynamics.
Physical Description: 77 p. : ill. ; 27 cm.
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