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Calculation of compressible flow in and about three-dimensional inlets with and without auxiliary inlets by a higher-order panel methodA three dimensional higher order panel method was specialized to the case of inlets with auxiliary inlets. The resulting program has a number of graphical input-output features to make it highly useful to the designer. The various aspects of the program are described instructions for its use are presented.
Document ID
19830003777
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hess, J. L.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Friedman, D. M.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:168009
MDC-J2548
NASA-CR-168009
Report Number: NAS 1.26:168009
Report Number: MDC-J2548
Report Number: NASA-CR-168009
Accession Number
83N12047
Funding Number(s)
CONTRACT_GRANT: NAS3-22147
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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