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Engineering considerations on the transversal contour of a lifting body.Lift drag ratios attainable by slender bodies at hypersonic speeds assuming modified Newtonian pressure distribution and surface constant friction coefficient
Document ID
19680041379
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Huang, H.-Y.
Miele, A.
Date Acquired
August 4, 2013
Publication Date
December 1, 1967
Publication Information
Publisher: JOURNAL OF THE ASTRONAUTICAL SCIENCES, VOL. 14, P. 262-269.
Subject Category
Aircraft
Meeting Information
Meeting: COLLOQUIUM ON ADVANCED PROBLEMS AND METHODS FOR SPACE FLIGHT OPTIMIZATION
Location: LIEGE
Country: BELGIUM
Start Date: January 1, 1967
Accession Number
68A22351
Funding Number(s)
CONTRACT_GRANT: NGR-44-006-063
Distribution Limits
Public
Copyright
Other

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