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- W2313502610 abstract "Combustion process in a scramjet has been stimulated by a quasi-one-dimensional model. Quasi-one-dimensional code has been validated by comparison with HyShot-2, Billing, Anderson and Queensland University experiments. The specific impulse for a typical hypersonic aircraft have been calculated. Development of two-dimensional model, has been focused on the SCHOLAR experiment. Convective and radiative heating the inner surface of the chamber scramjet have been studied by numerical simulation. The unsteady viscous-inviscid interacting flowfield and combustion of a hydrogen-air mixture in supersonic flow paths are modeled through thermo-physic gasdynamic code. Fields of chemical species concentrations, pressure, and temperature are calculated by twodimensional (axisymmetric and plane) computational model based on the unsteady governing equations including Navier-Stokes equations, energy conservation and diffusion equations together with system of chemical kinetic equations." @default.
- W2313502610 created "2016-06-24" @default.
- W2313502610 creator A5039017777 @default.
- W2313502610 creator A5072843540 @default.
- W2313502610 date "2015-07-23" @default.
- W2313502610 modified "2023-09-25" @default.
- W2313502610 title "Quasi-One-Dimensional and Two-Dimensional Numerical Simulation of Scramjet Combustors" @default.
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- W2313502610 doi "https://doi.org/10.2514/6.2015-4166" @default.
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