Taylor Maccoll Solution for Supersonic Flow over a Cone

Version 1.0.0 (4,82 ko) par Rohan Kokate
Taylor Maccoll Solution for Supersonic Flow over a Cone. The program solves for the entire flow field over the cone.
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Mise à jour 18 déc. 2020

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The following code provides a solution to solve the Taylor Maccoll equation for supersonic flow over a cone. The user needs to specify the freestream Mach number(M), the half cone angle (theta_cone), and the value of the ratio of specific heat (g). The solver specified below calls 4 sub-routines to solve the entire flowfield and provides all the important flow variables.
Reference: Fundamentals of Aerodynamics, J. D. Anderson.

Citation pour cette source

Rohan Kokate (2024). Taylor Maccoll Solution for Supersonic Flow over a Cone (https://www.mathworks.com/matlabcentral/fileexchange/84490-taylor-maccoll-solution-for-supersonic-flow-over-a-cone), MATLAB Central File Exchange. Récupéré le .

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Créé avec R2020b
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Version Publié le Notes de version
1.0.0