Prandtl Meyer Expansion fan solver function
Version 1.0.0 (1.72 KB) by
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.
Cite As
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. Retrieved .
MATLAB Release Compatibility
Created with
R2016b
Compatible with any release
Platform Compatibility
Windows macOS LinuxTags
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Version | Published | Release Notes | |
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1.0.0 |