Taylor Maccoll Solution for Supersonic Flow over a Cone

Versione 1.0.0 (4,82 KB) da Rohan Kokate
Taylor Maccoll Solution for Supersonic Flow over a Cone. The program solves for the entire flow field over the cone.
5.0
(1)
1,1K download
Aggiornato 18 dic 2020

Visualizza la licenza

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.

Cita come

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. Recuperato .

Compatibilità della release di MATLAB
Creato con R2020b
Compatibile con qualsiasi release
Compatibilità della piattaforma
Windows macOS Linux

Community Treasure Hunt

Find the treasures in MATLAB Central and discover how the community can help you!

Start Hunting!

Versione Pubblicato Note della release
1.0.0