Stagnation Pressure Effect on the Supersonic Two-Dimensional Plug Nozzle Design

The aim of this work is to develop a new calculation program to study the stagnation pressure effect of the combustion chamber on the design of the supersonic two-dimensional plug nozzle giving a uniform and parallel flow at the exit section. The model is based on the use of the real gas（RG） approac...

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Veröffentlicht in:	Transactions of Nanjing University of Aeronautics & Astronautics 2023-01, Vol.40 (1), p.1
Hauptverfasser:	Hamaidia, Walid, Yahiaoui, Toufik, Zebbiche, Toufik
Format:	Artikel
Sprache:	chi
Schlagworte:	Algorithms Combustion chambers Contours Convergence Density Design parameters Equations of state Exact solutions High temperature Ideal gas Mach number Mathematical models Nozzle design Parallel flow Plug nozzles Plugs Pressure effects Quadratures Real gases Robustness (mathematics) Stagnation pressure Stagnation temperature Vibration effects
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