1988
DOI: 10.1002/fld.1650081011
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Numerical simulation methods of incompressible flows and an application to the Space Shuttle main engine

Abstract: This paper discusses incompressible Navier‐Stokes solution methods with an emphasis on the pseudocompressibility method. A steady‐state flow solver based on the pseudocompressibility approach is then described. This flow solver code has been used to analyse the internal flow in the Space Shuttle main engine hot‐gas manifold. Salient features associated with this three‐dimensional realistic flow simulation are discussed. Numerical solutions relevant to the current engine analysis and the redesign effort are dis… Show more

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Cited by 31 publications
(17 citation statements)
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References 42 publications
(11 reference statements)
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“…Kwak et al [27], Chang et al [28], Choi and Merkle [29]). To obtain timedependent solutions using this method, an iterative procedure can be applied in each physical time step such that the continuity equation is satisfied.…”
Section: Artificial Compressibility Methodsmentioning
confidence: 99%
“…Kwak et al [27], Chang et al [28], Choi and Merkle [29]). To obtain timedependent solutions using this method, an iterative procedure can be applied in each physical time step such that the continuity equation is satisfied.…”
Section: Artificial Compressibility Methodsmentioning
confidence: 99%
“…Various applications that evolved from the artificial compressibility concept have been reported for obtaining steady-state solutions (e.g., Kwak et al [27], Chang et al [28], Choi and Merkle [29]). To obtain timedependent solutions using this method, an iterative procedure can be applied in each physical time step such that the continuity equation is satisfied.…”
Section: Artificial Compressibility Methodsmentioning
confidence: 99%
“…[27]), was developed using this scheme. The original A'S3D code was extensively used as a primary design tooi for an upgraded design of the Space Shurrie main engine (SSME) hor gas manifold by Chang et al [28]. This was probably the fmt major CFD contribution to rocket propulsion system design.…”
Section: Numerical Schemesmentioning
confidence: 99%
See 1 more Smart Citation
“…For example, the incompressible flow solver developed by Kwak et ai [1]was extensively used for simulating the flow through space shuttle main engine power head components. The redesign of the space shuttle main engine hot gas manifold, guided by the computations of Chang et al [2] illustrates the nsefullness of CFD in the aerospace research.…”
Section: Introductionmentioning
confidence: 99%