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- W2329122045 abstract "Aspects relating to the design, analysis, and optimization of scramjet engines for peak on and off-design performance are explored in this paper. Tip-to-tail flowpaths are developed and compared using both fixed and variable geometry combustors to assess their off-design penalties for Mach 8 and Mach 10 design points. The performance characterization is done for changes in Mach number, dynamic pressure, angle of attack, and fuel equivalence ratio. A quasi-one-dimensional engine model, including the effects of fuel injection location, mixing length, fuel mixing efficiency, chemical production rates, heat transfer, and viscous losses is utilized to assess the effects of hydrogen finite-rate chemistry. Due to the coupled nature of hypersonic propulsion/airframe integration, realistic two-dimensional inlet and nozzle designs have been included in this analysis." @default.
- W2329122045 created "2016-06-24" @default.
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- W2329122045 date "2004-06-26" @default.
- W2329122045 modified "2023-09-23" @default.
- W2329122045 title "Scramjet Optimization for Maximum Off-Design Performance" @default.
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- W2329122045 doi "https://doi.org/10.2514/6.2004-3343" @default.
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