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Experimental studies on the lip shock.Lip shock from separation edge of half angle wedge and resultant static pressure recovery distribution along wake
Document ID
19680035729
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hama, F. R.
Date Acquired
August 4, 2013
Publication Date
February 1, 1968
Publication Information
Publisher: AIAA JOURNAL, VOL. 6, P. 212-219.
Subject Category
Fluid Mechanics
Report/Patent Number
AIAA PAPER 67-29
Report Number: AIAA PAPER 67-29
Meeting Information
Meeting: AEROSPACE SCIENCES MEETING
Location: NEW YORK, NY
Start Date: January 23, 1967
End Date: January 26, 1967
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
68A16701
Distribution Limits
Public
Copyright
Other

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