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Three-dimensional, hypersonic wings of maximum lift-to-drag ratio.Three-dimensional slender wings of maximum lift/ drag ratio in hypersonic flow studied by variational calculus under several lift and volume conditions
Document ID
19670052235
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hull, D. G.
Miele, A.
Date Acquired
August 3, 2013
Publication Date
December 1, 1966
Publication Information
Publication: JOURNAL OF THE ASTRONAUTICAL SCIENCES
Subject Category
Aerodynamics
Accession Number
67A30964
Funding Number(s)
CONTRACT_GRANT: NGR-44-006-045
Distribution Limits
Public
Copyright
Other
Keywords
THREE-DIMENSIONAL FLOW
VARIATIONAL CALCULUS
HYPERSONIC FLOW
SLENDER WING
LIFT-DRAG RATIO

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