Prandtl Meyer Expansion fan solver function

A function made to solve supersonic Prandtl Meyer expansion fan with different input cases
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Mise à jour 30 oct. 2021

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This function solves Prandtl Meyer expansion using the relations given in "Modern Compressible Flow With Historical Prespective-John D. Anderson Jr"
  • It is only accurate in the range for mach number M=[1,7] because I used an approximate relation in one of the cases
  • You can solve for different cases depending on the given data for your problem, the values assigned for the flags determine the case you want to solve for.
  • variables names ending with 3 refer to the stream before expansion.
  • variables names ending with 4 refer to the stream after expansion.
  • I used 3 and 4 for consistency with an oblique shock function I created before this.

Citation pour cette source

Mohamed Hassan (2024). Prandtl Meyer Expansion fan solver function (https://www.mathworks.com/matlabcentral/fileexchange/101333-prandtl-meyer-expansion-fan-solver-function), MATLAB Central File Exchange. Récupéré le .

Compatibilité avec les versions de MATLAB
Créé avec R2016b
Compatible avec toutes les versions
Plateformes compatibles
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Version Publié le Notes de version
1.0.0