2019
DOI: 10.1017/aer.2019.42
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Stagnation pressure effect on the supersonic minimum length nozzle design

Abstract: The aim of this work is to develop a calculation model based on the method of characteristics making it possible to study the effect of the stagnation pressure of the combustion chamber on the 2D and axisymmetric minimum length nozzle design giving a uniform and parallel flow at the exit section. The model is based on the use of the real gas approach. The co-volume and the intermolecular interaction effect are taken into account by the use of the Berthelot state equation. The effect of molecular vibration is c… Show more

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Cited by 8 publications
(2 citation statements)
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“…The equations were discretized according to the finite difference method, and the second-order Euler predictor-corrector algorithm for the solutions (Shapiro, 1953;Zebbiche, 2019) of the operator points displayed in Fig. 4.…”
Section: Axisymmetric Flow Solutionmentioning
confidence: 99%
See 1 more Smart Citation
“…The equations were discretized according to the finite difference method, and the second-order Euler predictor-corrector algorithm for the solutions (Shapiro, 1953;Zebbiche, 2019) of the operator points displayed in Fig. 4.…”
Section: Axisymmetric Flow Solutionmentioning
confidence: 99%
“…This process is performed several times by employing Eqs. 4.110 to 4.113, until the maximum residual from the last iteration is lower than 10 −8 (Zebbiche, 2019).…”
Section: Axisymmetric Flow Solutionmentioning
confidence: 99%