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About this Engineering article
CFD Analysis of Hypersonic Combustion of H2-Fueled Scramjet Combustor with Cavity Based Fuel Injector at Flight Mach 6 by Pandey, Krishna Murari; Roga, Sukanta is a Engineering article available to read on EtoBox.
It is typically read by researchers, students, and practitioners in Engineering.
- Author
- Pandey, Krishna Murari; Roga, Sukanta
- Publisher
- Trans Tech Publications Inc.; Trans Tech Publications, Ltd.; Scitec Publications Ltd. (ISSN 1660-9336)
- Published
- 2014
- Language
- EN
- Field
- Engineering (Physical Sciences)