Parametric performance analysis of multiple reheat cycle for hydrogen fueled scramjet with multi-staged fuel injection
Author:
Publisher
Pleiades Publishing Ltd
Subject
Nuclear and High Energy Physics,Radiation
Link
https://link.springer.com/content/pdf/10.1134/S0869864321040120.pdf
Reference22 articles.
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3. F.S. Billig, Research on supersonic combustion, J. Propul-Power, 1993, Vol. 9, P. 499–514.
4. V.I. Zvegintsev, Gas-dynamic problems in off-design operation of supersonic inlets (review), Thermophysics and Aeromechanics, 2017, Vol. 24, No. 6, P. 807–834.
5. Y.P. Gounko and I.I. Mazhul, Gas-dynamic design of a two-dimensional supersonic inlet with the increased flow rate factor, Thermophysics and Aeromechanics, 2012, Vol. 19, No. 3, P. 363–379.
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1. Numerical Investigation of Flow Structures and Combustion Mechanisms with Different Injection Locations in a Hydrogen-Fueled Scramjet Combustor;Fire;2024-06-06
2. Thermophysical and physicochemical basis for hydrogen production in compact energy systems of low-carbon economy;Thermophysics and Aeromechanics;2024-02-13
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