Published 2004
| Version v1
Book
Investigation of Shock-Reflection Phenomena in over expanded Supersonic Jets
Creators
- 1. National Engineering and Scientific Commission, Islamabad (Pakistan)
Description
In order to validate our CFD Code PAK-3D, a study was made using PAK-3D. The study was to investigate Shock-Reflection Phenomena in over expanded Supersonic jets. In viscid computations were performed by Euler equations and transition from regular to Mach reflection and back was observed The results shows a hysteresis phenomenon as jet/ambient pressure ratio decreases and increases and the shock transition angle changes. (author)
Additional details
Publishing Information
- Publisher
- National Centre for Physics, Quaid-i-Azam Univ., Islamabad Pakistan
- Imprint Place
- Islamabad (Pakistan)
- Imprint Title
- Proceedings of international Bhurban conference on applied sciences and technology v. 1
- Imprint Pagination
- 500 p.
- Journal Page Range
- p. 432-439
Conference
- Title
- 3. International Bhurban conference on applied sciences and technology
- Dates
- 7-12 Jun 2004
- Place
- Islamabad (Pakistan)
INIS
- Country of Publication
- Pakistan
- Country of Input or Organization
- Pakistan
- INIS RN
- 36062303
- Subject category
- S70: PLASMA PHYSICS AND FUSION TECHNOLOGY;
- Resource subtype / Literary indicator
- Conference
- Descriptors DEI
- COMPUTERIZED SIMULATION; JETS; REFLECTION; SHOCK WAVES; SUPERSONIC FLOW
- Descriptors DEC
- FLUID FLOW; SIMULATION