Turbulent flow in supersonic and hypersonic nozzles

Turbulent flow in supersonic and hypersonic nozzles

The calculated turbulent flow properties in a supersonic or a hypersonic wind tunnel nozzle are affected by the location of laminar-turbulent transition point and the behavior of the particular turbulence models considered. A study numerically examined these effects by solving Reynolds-averaged Navi...

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Veröffentlicht in:AIAA journal 1995-09, Vol.33 (9), p.1634-1640
Hauptverfasser: Hu, Jiasen, Rizzi, Arthur
Format: Artikel
Sprache:eng
Schlagworte:
Aircraft
Compressible flows
shock and detonation phenomena
Exact sciences and technology
Fluid dynamics
Fundamental areas of phenomenology (including applications)
Physics
Supersonic and hypersonic flows
Turbulence
Wind tunnels
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Beschreibung
Zusammenfassung:The calculated turbulent flow properties in a supersonic or a hypersonic wind tunnel nozzle are affected by the location of laminar-turbulent transition point and the behavior of the particular turbulence models considered. A study numerically examined these effects by solving Reynolds-averaged Navier-Stokes equations for two nozzles.
ISSN:0001-1452
1533-385X
DOI:10.2514/3.12861