Performance Analysis of a Scramjet Combustor with Cavity for Mach Numbers 3.0, 3.25 and 3.50 with Hydrogen as a Fuel

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Performance Analysis of a Scramjet Combustor with Cavity for Mach Numbers 3.0, 3.25 and 3.50 with Hydrogen as a Fuel

Cited by 4 publications

References 18 publications

Impact of passive fuel injections techniques in the flow field of the scramjet combustor

Impact of passive fuel injections techniques in the flow field of the scramjet combustor

Computational Investigation of Transverse Fuel-Injection Scramjet Combustor for Different Incoming Mach Numbers

Computational Investigation to Interpret the Reacting Flow Conditions for Two Different Fuels in the Scramjet Combustor

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