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- W2316114584 abstract "support requirements and volumetric energy density considerations. The engine cycle and fuel choice pose unique challenges related to the jet-in-crossflow problem, and the design of a successful scramjet combustor remains one of the most challenging problems in supersonic aerodynamics. Among the many formidable tasks facing scramjet designers are the injection of fuel without introducing unacceptably large losses, the efficient mixing of the fuel with the freestream (where efficiency must be measured in terms of both time or distance and energy loss), the stabilization of a combustion region, and the management of heat transfer to walls and injector surfaces. Gaseous injection studies have investigated the effects of discharge orifice shapes (circular vs. elliptic), injector configurations (normal vs. angled, cascade, aeroramp), and different injectants (air vs. helium). The injection of pure and aerated liquids into high-speed crossflows has been studied. Liquid injection studies have investigated the fundamental breakup processes of liquid column, spray penetration height, and the effects of injection angle, liquid aeration, and injection conditions on spray structures." @default.
- W2316114584 created "2016-06-24" @default.
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- W2316114584 date "2005-01-10" @default.
- W2316114584 modified "2023-09-23" @default.
- W2316114584 title "Gaseous and Liquid Injection into High-speed Crossflows" @default.
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- W2316114584 doi "https://doi.org/10.2514/6.2005-301" @default.
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