Leading-to-trailing edge theoretical design of a generic scramjet

نویسندگان

چکیده

The aerospace vehicle flying at hypersonic speed, using an airbreathing propulsion system based on supersonic combustion (scramjet) technology, requires a highly integrated without moving parts, making the and shape indistinguishable. A scramjet uses shock waves, generated by its inlet during flight to provide temperature velocity of atmospheric air burn hydrogen, combustor speed. divergent exhaust nozzle accelerates products providing thrust. two-dimensional hydrogen-powered generic has been designed demonstrate in Mach number 6.8 altitude 30 km. Temperature chamber are most important key parameters for preliminary design. configuration must higher than ignition fuel guarantee spontaneous remain supersonics. exit should be obtain sustained produce enough For this theoretical analysis, is considered calorically perfect gas viscous effects. compressible flow analyzed oblique waves one-dimensional with friction heat addition Prandtl–Meyer coupled area ratio describe each component scramjet, such as compression, combustor, sections, respectively. mass hydrogen also critical design ensure stoichiometrically chamber, generating high

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ژورنال

عنوان ژورنال: AIP Advances

سال: 2022

ISSN: ['2158-3226']

DOI: https://doi.org/10.1063/5.0050786