Performance Improvement of DLR Scramjet Combustor Using Modified Strut Injector
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Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s13369-024-09013-6.pdf
Reference48 articles.
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3. Barber, M.J.; Schelz, J.A.; Roe, L.A.: Normal, sonic helium injection through a wedge-shaped orifice into supersonic flow. J. Propuls. Power. 13, 257–263 (1997). https://doi.org/10.2514/2.5157
4. Shan, F.; Hou, L.; Chen, Z.; Chen, J.; Wang, L.: Linearized correction to a flamelet-based model for hydrogen-fueled supersonic combustion. Int. J. Hydrogen Energy 42, 11937–11944 (2017). https://doi.org/10.1016/j.ijhydene.2017.02.100
5. Choubey, G.; Pandey, K.M.: Numerical studies on the performance of scramjet combustor with alternating wedge-shaped strut injector. Int. J. Turbo Jet Engines. 2015, 1–12 (2015). https://doi.org/10.1515/tjj-2015-0048
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