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Boundary-layer transition on sharp cones at hypersonic Mach numbers.Transition from laminar to turbulent boundary layer flow on sharp cones hypersonic Mach numbers, noting measurement techniques
Document ID
19680038867
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Henderson, A., Jr.
Maddalon, D. V.
Date Acquired
August 4, 2013
Publication Date
March 1, 1968
Publication Information
Publisher: AIAA JOURNAL, VOL. 6, P. 424-431.
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 67-130
Report Number: AIAA PAPER 67-130
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
68A19839
Distribution Limits
Public
Copyright
Other

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