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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 bodiesPressure distributions and drag coefficients of 18 constant length and volume slender bodies of revolution at zero incidence for Mach numbers 2.0 to 12.0 - graphs
Document ID
19710026940
Document Type
Other - NASA Technical Note (TN)
Authors
Stivers, L. S., Jr. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1971
Subject Category
AERODYNAMICS
Report/Patent Number
A-4005
NASA-TN-D-6536
Funding Number(s)
PROJECT: RTOP 760-75-01-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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