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- W2381141328 abstract "Numerical simulation of the inner supersonic compressible flow in a scramjet combustor with two cavities was carried out using upwind.The numerical simulation in cold state for Euler equations was carried out using the NND scheme to catch shocks and analyze shock characteristics clearly;Then,the numerical simulation in hydrogen spraying burning for Navier -Stokes equations was carried out using the third-order MUSCL scheme.A k-ω turbulence model was used with shear correction.It was concluded that stable flow and high speed mixing were obtained with two cavities,and the total pressure loss was higher for the cold state,but actual operation in the cavities resulted in lower total pressure loss,because mach numbers were decreased and shock intensities were reduced for the burning state." @default.
- W2381141328 created "2016-06-24" @default.
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- W2381141328 date "2007-01-01" @default.
- W2381141328 modified "2023-09-23" @default.
- W2381141328 title "Numerical Simulation of the Flow Field in Scramjet" @default.
- W2381141328 hasPublicationYear "2007" @default.
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