# Department of Aerospace Engineering
**Source**: https://ae.iitm.ac.in/aeweb/aerospace-dynamics.php
**Parent**: https://ae.iitm.ac.in/aeweb/innerfaculty.php?fname=Sriram
Combustion driven shock tunnel: Flows can be generated at Mach number ranges between 5-12 with Enthalpy levels upto 6 MJ. Both reflected and straight modes are possible, and can be used to study moving shock problems.- Title
- Department of Aerospace Engineering
- Category
- general
- UUID
79672553234c477da9ac4c979ecd5323
- Source URL
- https://ae.iitm.ac.in/aeweb/aerospace-dynamics.php
- Parent URL
- https://ae.iitm.ac.in/aeweb/innerfaculty.php?fname=Sriram
- Crawl Time
- 2026-03-17T07:05:25+00:00