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Hypersonic Flight MechanicsThe effects of aerodynamic forces on trajectories at orbital speeds are discussed in terms of atmospheric models. The assumptions for the model are spherical symmetry, nonrotating, and an exponential atmosphere. The equations of flight, and the performance in extra-atmospheric flight are discussed along with the return to the atmosphere, and the entry. Solutions of the exact equations using directly matched asymptotic expansions are presented.
Document ID
19760024112
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Busemann, A.
(Colorado Univ. Boulder, CO, United States)
Vinh, N. X.
(Colorado Univ. Boulder, CO, United States)
Culp, R. D.
(Colorado Univ. Boulder, CO, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1976
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-149170
Report Number: NASA-CR-149170
Accession Number
76N31200
Funding Number(s)
CONTRACT_GRANT: NSG-1056
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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