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- W2322425265 abstract "A two-dimensional flowfield analysis code for inlet flowfield studies has been developed. The methodology is valid from subsonic through hypersonic speeds. The code solves the Euler or Navier-Stokes equations with three gas models available: ideal gas, thermally perfect air, and equilibrium chemically reacting air. The governing equations are solved on zonal grids using an implicit, approximately factored, upwind scheme. Example solutions are shown from Mach 0.6 to 16.0 with comparisons to experimental data and other Computational Fluid Dynamics (CFD) codes." @default.
- W2322425265 created "2016-06-24" @default.
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- W2322425265 date "1987-06-29" @default.
- W2322425265 modified "2023-10-16" @default.
- W2322425265 title "Two-dimensional numerical analysis for inlets at subsonic through hypersonic speeds" @default.
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- W2322425265 doi "https://doi.org/10.2514/6.1987-1751" @default.
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