The Static Stability Characteristics Of Several Cone Cylinder Flare Cylinder Configurations At Mach Numbers 04 To 45
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The Static Stability Characteristics of Several Cone-cylinder-flare-cylinder Configurations at Mach Numbers 0.4 to 4.5
Author | : D. J. Spring |
Publisher | : |
Total Pages | : 270 |
Release | : 1963 |
Genre | : |
ISBN | : |
Download The Static Stability Characteristics of Several Cone-cylinder-flare-cylinder Configurations at Mach Numbers 0.4 to 4.5 Book in PDF, Epub and Kindle
The aerodynamic characteristics of various cone cylinder-flare-skirt configurations were inves tigated between Mach Numbers 0.4 to 4.5. The Reynolds number range for the tests was from 0.5 to 6.0 million per foot. Data are presented in basic form, along with cross plots, to show the effect of changing various body component shapes. (Author).
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