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- W2317202435 abstract "High speed flows over leading edge of hypersonic airfoil subject to an applied magnetic field is numerically simulated. The governing equations are composed of the Euler equation modified to include the effect of magnetic field. In the current applications, the low magnetic Reynolds number approximation is utilized. A four-stage modified Runge-Kutta scheme augmented with the Davis-Yee symmetric Total Variation Diminishing model in post-processing stage is used to solve the magnetogasdynamic equations. The flow simulations are compared to the existing solutions." @default.
- W2317202435 created "2016-06-24" @default.
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- W2317202435 date "2005-01-10" @default.
- W2317202435 modified "2023-09-25" @default.
- W2317202435 title "Numerical Investigation of Magnetogasdynamic High Speed Flows" @default.
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- W2317202435 doi "https://doi.org/10.2514/6.2005-1182" @default.
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