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Preliminary results from an experimental investigation of nozzle wall boundary layer at Mach numbers ranging from 27 to 47.Pressure and temperature surveys of Mach 27-47 nozzle boundary layer at Ames M-50 He tunnel, determining velocity profiles, wall friction coefficient, etc
Document ID
19690055452
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kemp, J. H., Jr.
Sreekanth, A. K.
Date Acquired
August 5, 2013
Publication Date
June 1, 1969
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Fluid Mechanics
Report/Patent Number
AIAA PAPER 69-686
Report Number: AIAA PAPER 69-686
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, FLUID AND PLASMA DYNAMICS CONFERENCE
Location: SAN FRANCISCO, CALIF.
Start Date: June 16, 1969
End Date: June 18, 1969
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A33441
Distribution Limits
Public
Copyright
Other

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