39th Aerospace Sciences Meeting and Exhibit 2001
DOI: 10.2514/6.2001-744
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Prediction of shock-cell structure using parabolized stability equations

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Cited by 4 publications
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“…Assuming constant static pressure, fixed stagnation temperature and known jet centreline temperature the density was found from the equation of state of an ideal gas. The reference solution used in the sponge zones was found from Reynolds-averaged Navier-Stokes solutions of the parabolized Navier-Stokes equations, using the v 2 -f turbulence model (Choi & Lele 2001). A schematic of the computational domain, with sponge zones identified, is given in figure 1.…”
Section: Discussionmentioning
confidence: 99%
“…Assuming constant static pressure, fixed stagnation temperature and known jet centreline temperature the density was found from the equation of state of an ideal gas. The reference solution used in the sponge zones was found from Reynolds-averaged Navier-Stokes solutions of the parabolized Navier-Stokes equations, using the v 2 -f turbulence model (Choi & Lele 2001). A schematic of the computational domain, with sponge zones identified, is given in figure 1.…”
Section: Discussionmentioning
confidence: 99%