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• W2012103487 abstract "A review of past and current research applicable to liquid-fueled supersonic combustion ramjets is presented and discussed. An assessment of its strengths and shortcomings is made and, finally, a list of research opportunities that merit consideration in this rapidly expanding area of airbreathing propulsion is presented. Nomenclature = area Cf = average combustor wall skin friction coefficient D = isolator duct diameter d = injector diameter ER = fuel-air equivalence ratio / = fuel-air ratio h - penetration height, enthalpy Ah = driving enthalpy (Ref. 85) M -Mach number P = static pressure q = fuel-to-freestream dynamic pressure ratio, average q = combustor wall heat flux Ree = Reynolds number based on momentum thickness Sd = length of precombustion shock structure in supersonic combustion Ss = total length of precombustion shock structure T = temperature w =fuel jet lateral spreading w =mass flow rate x = axial distance downstream of injection 6 =fuel injection angle 6m = boundary-layer momentum thickness r/c =heat release combustion efficiency f = average combustor skin friction" @default.
• W2012103487 created "2016-06-24" @default.
• W2012103487 creator A5037184077 @default.
• W2012103487 date "1987-11-01" @default.
• W2012103487 modified "2023-09-23" @default.
• W2012103487 title "Liquid-fueled supersonic combustion ramjets - A research perspective" @default.
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• W2012103487 doi "https://doi.org/10.2514/3.23019" @default.
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