NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Comparison of experimental and theoretical shock shapes and pressure distributions on flat-faced cylinders at Mach 10.5Integer relations method of determining inviscid shock layer flow and pressure distributions over blunt bodies
Document ID
19680006309
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Inouye, M. (NASA Ames Research Center Moffett Field, CA, United States)
Marvin, J. G. (NASA Ames Research Center Moffett Field, CA, United States)
Sinclair, A. R. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1968
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4397
Report Number: NASA-TN-D-4397
Accession Number
68N15778
Funding Number(s)
CONTRACT_GRANT: 129-01-09-01-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available