NASA technical notes TN (series). D-1781. Effects of nose bluntness, fineness ratio, cone angle, and model base on static aerodynamic characteristics of blunt bodies at Mach numbers of 1.57, 1.80, and 2.16 and angles of attack up to 180° [with list of references]; by David S. Shaw, Dennis E. Fuller, and C. Donald Babb.
Publication Title:
Effects of nose bluntness, fineness ratio, cone angle, and model base on static aerodynamic characteristics of blunt bodies at Mach numbers of 1.57, 1.80, and 2.16 and angles of attack up to 180° [with list of references]; by David S. Shaw, Dennis E. Fuller, and C. Donald Babb.
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NASA technical notes TN (series). D-1781. Effects of nose bluntness, fineness ratio, cone angle, and model base on static aerodynamic characteristics of blunt bodies at Mach numbers of 1.57, 1.80, and 2.16 and angles of attack up to 180° [with list of references]; by David S. Shaw, Dennis E. Fuller, and C. Donald Babb.
Series Title:
NASA technical notes TN (series).
Corporate Agency Authors:
National Aeronautics and Space Administration
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National Aeronautics and Space Administration
Authors:
Shaw, David S., Fuller, Dennis E., and Babb, C. Donald