Published 2004
| Version v1
Book
Shock stand off Calculations for Hemisphere in Hypersonic Flows
- 1. National Engineering and Scientific Commission, Islamabad (Pakistan)
Description
The shape and location of shock has been studied by solving the axi symmetric Navier Stokes Equations for a hemisphere in hypersonic flow. The effect of Mach number on shock stand-off distance has been investigated. It is found that the shock location varies with Mach number and the free stream conditions at a given nose radius. (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. 414-425
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
- 36062301
- Subject category
- S71: CLASSICAL AND QUANTUM MECHANICS, GENERAL PHYSICS;
- Resource subtype / Literary indicator
- Conference
- Descriptors DEI
- AXIAL SYMMETRY; HYPERSONIC FLOW; MACH NUMBER; MATHEMATICAL SOLUTIONS; NAVIER-STOKES EQUATIONS; SHOCK WAVES
- Descriptors DEC
- DIFFERENTIAL EQUATIONS; DIMENSIONLESS NUMBERS; EQUATIONS; FLUID FLOW; PARTIAL DIFFERENTIAL EQUATIONS; SYMMETRY; VELOCITY