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Steady and fluctuating pressures at transonic speeds on two space-vehicle payload shapesTransonic wind tunnel tests on Centaur and Able V models for steady and fluctuating pressure measurement
Document ID
19650018342
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Coe, C. F.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1962
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-503
Report Number: NASA-TM-X-503
Accession Number
65N27943
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLUCTUATION THEORY /STAT MECH/
STEADY FLOW
PRESSURE MEASUREMENT
CENTAUR LAUNCH VEHICLE
TRANSONIC WIND TUNNEL
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