Numerical simulations of single and multi-staged injection of H2 in a supersonic scramjet combustor

Author:

Abu-Farah L.,Haidn O.J.,Kau H.-P.

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Fuel Technology,Aerospace Engineering,Automotive Engineering

Reference21 articles.

1. D. G. Andrew, J. E. Andrews, Designing for the future space transportation missions, in: The 37th Joint Propulsion Conference and Exhibit, AIAA-2001-3964, 2001.

2. D. Maier, S. Kirstein, T. Fuhrmann, S.R. Denis, A. Hupfer, H.P. Kau, Scramjet research activities at the institute of flight propulsion of the Techniche Unversitaet Muenchen, in: The 6th European Symposium on Aerothermodynamics for Space Vehicles, Versailles, France, 3–6, November, 2008.

3. CFD analysis of mixing and combustion of a scramjet combustor with a planer strut injector;Pandey;International Journal of Environmental Science and Development,2011

4. CFD analysis of hydrogen fuelled mixture in scramjet combustor with a strut injector by using fluent software;Pandey;International Journal of Engineering and Technology,2011

5. Numerical investigation of mixing and combustion enhancement in supersonic combustors by strut induced stream vorticity;Gerlinger;Aerospace Science and Technology,2008

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