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An experimental investigation of hypersonic turbulent boundary layers in adverse pressure gradient.Hypersonic turbulent boundary layer in adverse pressure gradients studied for transition, measuring static/pitot pressure, stagnation temperature and heat transfer rates
Document ID
19690036727
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hoydysh, W. G.
Zakkay, V.
Date Acquired
August 5, 2013
Publication Date
January 1, 1969
Subject Category
Fluid Mechanics
Report/Patent Number
AIAA PAPER 68-44
Report Number: AIAA PAPER 68-44
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AEROSPACE SCIENCES MEETING
Location: NEW YORK, NY
Start Date: January 22, 1968
End Date: January 24, 1968
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A14716
Funding Number(s)
CONTRACT_GRANT: NGR-33-016-067
Distribution Limits
Public
Copyright
Other

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