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Mach reflection from overexpanded nozzle flows.
- Source :
- AIAA Journal. 10
- Publication Year :
- 1972
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1972.
-
Abstract
- Investigation of the Mach reflection associated with a steady two-dimensional overexpanded nozzle flow. The conditions of occurrence of triple point shock configuration are described, and Mach reflection configurations for two values of the incident shock are presented, along with the Mach stem height variation for different Mach numbers under conditions of different pressure ratios.
- Subjects :
- Aerodynamics
Subjects
Details
- Language :
- English
- Volume :
- 10
- Database :
- NASA Technical Reports
- Journal :
- AIAA Journal
- Notes :
- NGL-14-005-140
- Publication Type :
- Report
- Accession number :
- edsnas.19720062128
- Document Type :
- Report