27th Thermophysics Conference 1992
DOI: 10.2514/6.1992-2898
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A three-dimensional upwind PNS code for chemically reacting scramjetflowfields

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Cited by 1 publication
(4 citation statements)
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“…Two test cases were chosen to demonstrate and validate the hydrogen-air combustion model as well as the three-dimensional internal flow capability of the code with algebraic turbulence modeling [37]. These test cases are typical of portions of the flowfield in the scramjet engine of a hypersonic vehicle.…”
Section: Numerical Results and Discussionmentioning
confidence: 99%
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“…Two test cases were chosen to demonstrate and validate the hydrogen-air combustion model as well as the three-dimensional internal flow capability of the code with algebraic turbulence modeling [37]. These test cases are typical of portions of the flowfield in the scramjet engine of a hypersonic vehicle.…”
Section: Numerical Results and Discussionmentioning
confidence: 99%
“…A^^th the algebraic turbulence model employed, the code is applied to two internal flow test cases [37]. These test cases model portions of the flowfield in a typical scramjet engine of a hypersonic vehicle.…”
Section: Current Workmentioning
confidence: 99%
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