Prandtl Meyer Expansion fan solver function
Versione 1.0.0 (1,72 KB) da
Mohamed Hassan
A function made to solve supersonic Prandtl Meyer expansion fan with different input cases
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.
Cita come
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. Recuperato .
Compatibilità della release di MATLAB
Creato con
R2016b
Compatibile con qualsiasi release
Compatibilità della piattaforma
Windows macOS LinuxTag
Community Treasure Hunt
Find the treasures in MATLAB Central and discover how the community can help you!
Start Hunting!Scopri Live Editor
Crea script con codice, output e testo formattato in un unico documento eseguibile.
Versione | Pubblicato | Note della release | |
---|---|---|---|
1.0.0 |