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A method for predicting shock shapes and pressure distributions for a wide variety of blunt bodies at zero angle of attackRelationship of shock standoff distance, at sonic and stagnation points, to body geometry of blunt bodies at zero angle of attack
Document ID
19680012472
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Kaattari, G. E. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4539
Report Number: NASA-TN-D-4539
Accession Number
68N21941
Funding Number(s)
CONTRACT_GRANT: 129-01-08-01-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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