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Conical shock-wave turbulent boundary-layer interaction including suction effectsConical shock wave-turbulent boundary layer interaction data obtained for adiabatic wall conditions at supersonic free stream Mach numbers, including suction effects
Document ID
19700060332
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Childs, M. E.
Seebaugh, W. R.
Date Acquired
August 5, 2013
Publication Date
August 1, 1970
Subject Category
Fluid Mechanics
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE, 5TH, U.S. AIR FORCE ACADEMY
Location: COLORADO SPRINGS, CO
Start Date: June 9, 1969
End Date: June 13, 1969
Sponsors: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
70A36448
Distribution Limits
Public
Copyright
Other

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