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A highly efficient engineering tool for three-dimensional scramjet flowfield and heat transfer computationsThe SIMPLE-based parabolic flow code, SHIP3D, was under development for use as a parametric design and analysis tool for scramjets. Some capabilities and applications of the code are demonstrated, and a report on its current status is given. The focus is on the combustor for which the code was mostly used. Recently, it was also applied to nozzle flows. Code validation results are presented for combustor unit problems involving film cooling, transverse fuel injection, and nozzle test. A parametric study of a film cooled or transpiration cooled Mach 16 combustor is also conducted to illustrate the application of the code to a design problem.
Document ID
19910011785
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kamath, Pradeep S.
(Analytical Services and Materials, Inc., Hampton VA., United States)
Hawkins, Richard W.
(Analytical Services and Materials, Inc., Hampton VA., United States)
Baker, Nathaniel R.
(Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Mcclinton, Charles R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: NASA, Lewis Research Center, Computational Fluid Dynamics Symposium on Aeropropulsion
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
91N21098
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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