A THREE-DIMENSIONAL INCOMPRESSIBLE PLOW SIMULATION METHOD AND ITS APPLICATION TO THE SPACE SHUTTLE MAIN ENGINE - Part I - Laminar Flow

Chang, J. L. C.; Kwak, Dochan; Dao, S. C.; Rosen, Robert

doi:10.2514/6.1985-175

Cited by 16 publications

(2 citation statements)

References 4 publications

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“…which is a non-linear function, and q k are the stencils as in Equations (10) and (11). The numerical fluxes obtained in each characteristic field can be projected back to the physical space by (here only the two-dimensional case is described)…”

Section: Spatial Discretizationmentioning

confidence: 99%

Implicit weighted essentially non-oscillatory schemes for the incompressible Navier-Stokes equations

Chen

Yang

1999

Int. J. Numer. Meth. Fluids

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Section: Spatial Discretizationmentioning

confidence: 99%

Implicit weighted essentially non-oscillatory schemes for the incompressible Navier-Stokes equations

Chen

Yang

1999

Int. J. Numer. Meth. Fluids

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“…The values of floin is computed locally but otherwise, the time marching compressible code remains 'standard' as described by Ng, 1994 (Part 1). Many researchers have their own value of the acoustic speed, fi For examples; Choi et al (1984) concluded that numerical experiments indicate flop: 1 u 2 near unity was optimal for best convergence rate whereas Chang et al (1985) used lower and upper bounds of Pope /u2 according to the Reynolds number and the geometry in between the values of 0.1 and 10. In this work, we defined the optimum artificial acoustic speed (after Walker (1988)) as Sop = 2.14 u 2 / (1-M 2 ) which is equivalent to assuming a modified equation of state for the gas, p = P p. The present approach is only valid for steady flow.…”

Section: Op = P • Opmentioning

confidence: 99%

Prediction of 3-D Viscous Flow of Centrifugal Impeller With Tip-Clearance: Part 2 — Mixed-Flow Water Pump

1997

ASME 1997 Turbo Asia Conference

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This paper describes an extension of 3D time-marching compressible Navier-Stokes solver (Part 1) for an incompressible application through the pseudo-compressibility technique suggested by Chorin. Effect of tip clearances on the mixed-flow pump is investigated. Static pressure distribution and intricate internal flow pattern is reasonably well predicted. Fine-tuning of the pseudo-compressibility parameter and grid size is required for improve convergence and stability.

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Computation of internal turbulent flow with a large separated flow region

Kaul

Kwak

1986

Numerical Methods in Fluids

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SUMMARYAn implicit two-equation turbulence solver, KEM, in generalized co-ordinates, is used in conjunction with the three-dimensional incompressible Navier-Stokes solver, INS3D, to calculate the internal flow in a channel and a channel with a sudden 2:3 expansion. A new and consistent boundary procedure for a low Reynolds number form of the k--E turbulence model is chosen to integrate the equations up to the wall. The high Reynolds number form of the equations is integrated using wall functions. The latter approach yields a faster convergence to the steady-state solution than the former. For the case of channel flow, both the wall-function and wall-boundary-condition approaches yield results in good agreement with the experimental data. The back-step (sudden expansion) flow is calculated using the wall-function approach. The predictions are in reasonable agreement with the experimental data.

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A THREE-DIMENSIONAL INCOMPRESSIBLE PLOW SIMULATION METHOD AND ITS APPLICATION TO THE SPACE SHUTTLE MAIN ENGINE - Part I - Laminar Flow

Cited by 16 publications

References 4 publications

Implicit weighted essentially non-oscillatory schemes for the incompressible Navier-Stokes equations

Implicit weighted essentially non-oscillatory schemes for the incompressible Navier-Stokes equations

Prediction of 3-D Viscous Flow of Centrifugal Impeller With Tip-Clearance: Part 2 — Mixed-Flow Water Pump

Computation of internal turbulent flow with a large separated flow region

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