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Massive blowing effects on viscous, radiating, stagnation-point flowMassive blowing effect on stagnation point radiative energy transfer of ablative heat shield during planetary entry at hypersonic velocities
Document ID
19700041985
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wilson, K. H.
Date Acquired
August 5, 2013
Publication Date
January 1, 1970
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 70-203
Report Number: AIAA PAPER 70-203
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AEROSPACE SCIENCES MEETING, 8TH
Location: NEW YORK, NY
Start Date: January 19, 1970
End Date: January 21, 1970
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
70A18101
Funding Number(s)
CONTRACT_GRANT: NAS7-632
Distribution Limits
Public
Copyright
Other

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