Stagnation Temperature Effect on the Prandtl Meyer Function
The Prandtl Meyer (PM) function plays a significant role in the supersonic flows calculation. To design a supersonic nozzle giving a uniform and parallel flow at the exit section [1-3], it is necessary to deviate the nozzle at the throat of an initial expansion angle to have the desired exit Mach nu...
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| Veröffentlicht in: | AIAA journal 2007-04, Vol.45 (4), p.952-954 |
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| creator | Zebbiche, Toufik |
| description | The Prandtl Meyer (PM) function plays a significant role in the supersonic flows calculation. To design a supersonic nozzle giving a uniform and parallel flow at the exit section [1-3], it is necessary to deviate the nozzle at the throat of an initial expansion angle to have the desired exit Mach number. Zebbiche features the new Prandtl Meyer function form, presented by integration of a complex analytical function, where the analytical calculation procedure is impossible. The interest then is oriented to the determination of the approximate numerical solutions. [PUBLICATION ABSTRACT] |
| doi_str_mv | 10.2514/1.24868 |
| format | Article |
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| fulltext | fulltext |
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| ispartof | AIAA journal, 2007-04, Vol.45 (4), p.952-954 |
| issn | 0001-1452 1533-385X |
| language | eng |
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| source | Alma/SFX Local Collection |
| subjects | Aerodynamics Air flow Compressible flows shock and detonation phenomena Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Physics Shock-wave interactions and shock effects Temperature Temperature effects Turbulent flow |
| title | Stagnation Temperature Effect on the Prandtl Meyer Function |
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