Cover image for Calculated pressure distributions and components of total-drag coefficients for 18 constant-volume slender bodies of revolution at zero incidence for Mach numbers from 2.0 to 12.0, with experimental aerodynamic characteristics for three of the bodies
Title:
Calculated pressure distributions and components of total-drag coefficients for 18 constant-volume slender bodies of revolution at zero incidence for Mach numbers from 2.0 to 12.0, with experimental aerodynamic characteristics for three of the bodies
Author:
Stiver, Louis S.
Personal Author:
Publication Information:
Washington, D.C. : National Aeronautics and Space Administration, 1971.
Physical Description:
iv, 96 pages : illustrations ; 27 cm.
General Note:
N71-36416.

Prepared at Ames Research Center.
Language:
English
Format :
Book

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TL507 .U565 D6536-6545 D6536 Adult Non-Fiction Central Closed Stacks-Non circulating
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