25th AIAA Aerospace Sciences Meeting 1987
DOI: 10.2514/6.1987-601
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Three-dimensional viscous flow solutions with a vorticity-stream function formulation

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Cited by 7 publications
(9 citation statements)
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“…Figure 21 show comparisons of the pressure p -%(!-ùj) where is the velocity at the edge of the boundary layer, with the results of Veldman (1981) who studied the same configuration using a quasi-simultaneous viscous-inviscid interaction procedure. The present results are compared with those of Veldman because Davis et al (1986) did not present values of the pressure in their report. The figure shows good agreement between the present boundary-layer results and that of Veldman.…”
Section: ^ Results and Discussionmentioning
confidence: 75%
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“…Figure 21 show comparisons of the pressure p -%(!-ùj) where is the velocity at the edge of the boundary layer, with the results of Veldman (1981) who studied the same configuration using a quasi-simultaneous viscous-inviscid interaction procedure. The present results are compared with those of Veldman because Davis et al (1986) did not present values of the pressure in their report. The figure shows good agreement between the present boundary-layer results and that of Veldman.…”
Section: ^ Results and Discussionmentioning
confidence: 75%
“…Related methods have been presented by Davis et al (1986) who used the decom position of the velocity field into two stream functions and applied it to compute the incompressible viscous flow over three-dimensional troughs and bumps. An excellent review of the techniques used for solving the Navier-Stokes equations in two dimensions with the vorticity/stream-function method is given by Roache (1972).…”
Section: Incompressible Flowmentioning
confidence: 99%
“…External viscous flows have been computed by Davis et al (1989). No attempts have been reported on the use of this method to solve three-dimensional unsteady compressible viscous flows.…”
Section: Dual Potential Approachmentioning
confidence: 99%
“…Some viscous external flow solutions were obtained by Rao (1987) and Davis et al (1986) for flow over two-and three-dimensional troughs. Rao (1987) used interacting boundary layer theory to supply the vorticity to a dual potential code for the inviscid rotational part of the flow.…”
Section: Dual Potential Approachmentioning
confidence: 99%
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