NASA NTRS · 19910011785
A highly efficient engineering tool for three-dimensional scramjet flowfield and heat transfer computations
Abstract
The 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.
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Kamath, Pradeep S., Hawkins, Richard W., Baker, Nathaniel R., Mcclinton, Charles R.. 1991-01-01. A highly efficient engineering tool for three-dimensional scramjet flowfield and heat transfer computations. https://ntrs.nasa.gov/citations/19910011785
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