Good example showing how to perform gas dynamic calculations in MATLAB.
| Date | Contributor | Description | Rating |
|---|---|---|---|
| 29 Mar 2010 | Stacey Gage |
This demo illustrates how to use the method of characteristics and Prandtl-Meyer flow theory to solve a problem in supersonic flow involving expansions. Solve for the flow field downstream of the exit of a supersonic nozzle. |
| Tag | Applied By | Date/Time |
|---|---|---|
| computational methods | MathWorks Classroom Resources Team | 31 Mar 2010 at 5:12pm |
| course materials | MathWorks Classroom Resources Team | 31 Mar 2010 at 5:12pm |
| language english | MathWorks Classroom Resources Team | 31 Mar 2010 at 5:11pm |
| aerospace engineering | MathWorks Classroom Resources Team | 31 Mar 2010 at 5:11pm |
| academic | MathWorks Classroom Resources Team | 31 Mar 2010 at 5:11pm |
| academic | Stacey Gage | 29 Mar 2010 at 4:39pm |
| gas dynamics | Stacey Gage | 29 Mar 2010 at 4:39pm |
| language english | Stacey Gage | 29 Mar 2010 at 4:39pm |
| course materials | Stacey Gage | 29 Mar 2010 at 4:39pm |
| aerospace engineering | Stacey Gage | 29 Mar 2010 at 4:39pm |
| project based learning | Stacey Gage | 29 Mar 2010 at 4:39pm |
| computational methods | Stacey Gage | 29 Mar 2010 at 4:39pm |