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A Fortran computer code for the calculation of unsteady supersonic flow field by the method of perturbationFortran computer code for analysis of unsteady supersonic flow field around oscillating body of revolution
Document ID
19680006378
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hsu, P.-T. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
August 4, 2013
Publication Date
September 1, 1967
Subject Category
Fluid Mechanics
Report/Patent Number
REPT.-67-3
NASA-CR-61493
Report Number: REPT.-67-3
Report Number: NASA-CR-61493
Accession Number
68N15847
Funding Number(s)
CONTRACT_GRANT: NAS8-873
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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