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Utilization of the wing-body aerodynamic analysis programThe analysis program was used to investigate several aircraft characteristics. The studies performed included vehicle stability analysis, determination of upwash angle, identification of nonpotential flow, launch dynamics, and wake vortex upset loads. The techniques and are discussed. When possible, computed results are compared with experimental data.
Document ID
19790001849
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Curry, R. E.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1978
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-72856
H-1071
Report Number: NASA-TM-72856
Report Number: H-1071
Accession Number
79N10020
Funding Number(s)
PROJECT: RTOP 505-06-54
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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