Wind tunnel tests of a hydrogen-fueled detonation ramjet model at approach air stream Mach numbers from 4 to 8 - Concepedia

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Wind tunnel tests of a hydrogen-fueled detonation ramjet model at approach air stream Mach numbers from 4 to 8

74

Citations

17

References

2017

Year

V. S. Ivanov, V. S. Aksenov, D. A. Vnuchkov, D. G. Nalivaichenko

International Journal of Hydrogen Energy

EngineeringDetonation PhenomenonAerospace EngineeringWind Tunnel TestsAerodynamicsPropulsionAerospace Propulsion SystemsAerospace Propulsion

References

	Year	Citations

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