Hydrogen-fueled detonation ramjet model: Wind tunnel tests at approach air stream Mach number 5.7 and stagnation temperature 1500 K - Concepedia

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Hydrogen-fueled detonation ramjet model: Wind tunnel tests at approach air stream Mach number 5.7 and stagnation temperature 1500 K

78

Citations

29

References

2018

Year

V. S. Ivanov, V. S. Aksenov, D. A. Vnuchkov, D. G. Nalivaichenko, A.A. Berlin, A. N. Shiplyuk, N. N. Yakovlev

International Journal of Hydrogen Energy

EngineeringDetonation PhenomenonAerospace EngineeringWind Tunnel TestsAerodynamicsStagnation Temperature 1500PropulsionAerospace PropulsionHydrogen Combustion

References

	Year	Citations

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