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Unusual boundary-layer transition results on cones in hypersonic flow.Subliming ablation effects on boundary layer transition for cones in hypersonic flow, discussing Reynolds numbers measured in wind tunnel tests
Document ID
19680036492
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Larson, H. K.
Mateer, G. G.
Date Acquired
August 4, 2013
Publication Date
January 1, 1968
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS.
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 68-40
Report Number: AIAA PAPER 68-40
Meeting Information
Meeting: 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
68A17464
Distribution Limits
Public
Copyright
Other

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