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COMPARISON OF CALCULATED WITH MEASURED BOUNDARY-LAYER THICKNESSES ON THE CURVED WALLS OF THE JPL 20-IN. SUPERSONIC WIND TUNNEL TWODIMENSIONAL NOZZLEBoundary layer thickness on curved walls of 20-in supersonic wind tunnel two-dimensional nozzle
Document ID
19630013774
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dayman, B., Jr. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 18, 1963
Subject Category
Electronics
Report/Patent Number
JPL-IR-32-349
NASA-CR-52252
Report Number: JPL-IR-32-349
Report Number: NASA-CR-52252
Accession Number
63N23654
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TWO-DIMENSIONAL BODY
SUPERSONIC WIND TUNNEL APPARATUS
BOUNDARY LAYER
NOZZLE WALL

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