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Experimental program to investigate transonic flow around protuberancesTransient and steady state aerodynamic flow of turbulent boundary layers are investigated for generalized cylindrical projections and several specific configurations used on the Saturn 5 launch vehicle. A transonic wind tunnel gave generalized information.
Document ID
19690000563
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Robertson, J. E.
Date Acquired
August 5, 2013
Publication Date
November 1, 1969
Subject Category
Mechanics
Report/Patent Number
MFS-20037
Report Number: MFS-20037
Accession Number
69B10609
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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