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Nasa Technical Reports Server (ntrs) 19940014080%3a A Comparative Study Of Turbulence Models In Predicting Hypersonic Inlet Flows by Nasa Technical Reports Server (ntrs)
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1NASA Technical Reports Server (NTRS) 19940014080: A Comparative Study Of Turbulence Models In Predicting Hypersonic Inlet Flows
By NASA Technical Reports Server (NTRS)
A computational study has been conducted to evaluate the performance of various turbulence models. The NASA P8 inlet, which represents cruise condition of a typical hypersonic air-breathing vehicle, was selected as a test case for the study; the PARC2D code, which solves the full two dimensional Reynolds-averaged Navier-Stokes equations, was used. Results are presented for a total of six versions of zero- and two-equation turbulence models. Zero-equation models tested are the Baldwin-Lomax model, the Thomas model, and a combination of the two. Two-equation models tested are low-Reynolds number models (the Chien model and the Speziale model) and a high-Reynolds number model (the Launder and Spalding model).
“NASA Technical Reports Server (NTRS) 19940014080: A Comparative Study Of Turbulence Models In Predicting Hypersonic Inlet Flows” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19940014080: A Comparative Study Of Turbulence Models In Predicting Hypersonic Inlet Flows
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19940014080: A Comparative Study Of Turbulence Models In Predicting Hypersonic Inlet Flows” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - COMPUTATIONAL FLUID DYNAMICS - DENSITY DISTRIBUTION - HYPERSONIC INLETS - INLET FLOW - MACH NUMBER - PRESSURE DISTRIBUTION - STAGNATION TEMPERATURE - TURBULENCE MODELS - TURBULENT FLOW - BOUNDARY LAYERS - HIGH REYNOLDS NUMBER - LOW REYNOLDS NUMBER - NAVIER-STOKES EQUATION - SHOCK WAVE INTERACTION - WIND TUNNEL TESTS - Kapoor, Kamlesh
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19940014080
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