11th Fluid and PlasmaDynamics Conference 1978
DOI: 10.2514/6.1978-1137
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Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges

Abstract: Vigneron, Yvon Clovis, "Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges " (1978). 4. The majority of users indicate that the textual content is of greatest value, however, a somewhat higher quality reproduction could be made from "photographs" if essential to the understanding of the dissertation. Silver

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Cited by 166 publications
(58 citation statements)
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“…The final form of the governing equations becomes DE* + a n + a ^ (4) An eigenvalue analysis shows that this system will be hyperbolic-parabolic…”
Section: Parabolizing Assumptionsmentioning
confidence: 99%
“…The final form of the governing equations becomes DE* + a n + a ^ (4) An eigenvalue analysis shows that this system will be hyperbolic-parabolic…”
Section: Parabolizing Assumptionsmentioning
confidence: 99%
“…Nonlinearity enters in the single level space marching form (4) in that at each step of the forward sweep the matrices X+ are averag'!d between q'i-l and qj rather than homogeneously at the old iteration level n. Simila.ly, companion bach.--ward space marching sweep that is symmetric to equation (4) and that is intimately related to the backward sweep of the alternating bidiagonal algorithm of reference (10) is…”
Section: Quasi Lad Formulationmentioning
confidence: 99%
“…A tangency boundary condition was imposed on solid walls for the Euler solutions, while a no-slip boundary condition with a fixed wall temperature of 90 degrees Fahrenheit was imposed for PNS solutions. Additionally, the Vigneron technique was utilized in PNS solutions to eliminate the streamwise pressure gradients in subsonic portions of the boundary layer, which prevents the solution from diverging 9 .…”
Section: D Proceduresmentioning
confidence: 99%