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The computation of supersonic flow fields about wing-body combinations by 'shock-capturing' finite difference techniquesSupersonic flow field computation for wing-body combinations by shock-capturing finite difference techniques, discussing improvement based on Runge-Kutta method
Document ID
19710055606
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kutler, P.
Lomax, H.
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Publication Information
Publisher: SPRINGER- VERLAG,
Subject Category
Aerodynamics
Meeting Information
Meeting: INTERNATIONAL CONFERENCE ON NUMERICAL METHODS IN FLUID DYNAMICS
Location: BERKELEY, CA
Start Date: September 15, 1970
End Date: September 19, 1970
Accession Number
71A36303
Distribution Limits
Public
Copyright
Other

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