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1

Digitale Medien

Navier-Stokes simulation of flow through a highly contoured subsonic diffuser (1992)

Chyu, W. J. ; Bencze, D. P.

Chichester [u.a.] : Wiley-Blackwell

International Journal for Numerical Methods in Engineering 34 (1992), S. 473-483

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ISSN: 0029-5981

Schlagwort(e): Engineering ; Engineering General

Quelle: Wiley InterScience Backfile Collection 1832-2000

Thema: Mathematik , Technik allgemein

Notizen: The flow through a highly offset subsonic diffuser with cross-sectional profiles that varied from rectangular at the duct entrance to circular a t the engine face was numerically simulated. A multizonal approach combined with a two-grid topology was used to represent both the internal and external flow fields, and an implicit, approximately-factored, partially flux-split finite-difference algorithm was used to solve the three-dimensional thin-layer Navier-Stokes equations. The computed static pressures along the inlet wall and total pressures on the engine face were compared with experimental data. In addition, the overall flow field within the duct was examined in detail. Good agreement is shown between experiment and computations, with the limiting factor being the lack of a reliable turbulence model for internal flow problems.

Zusätzliches Material: 7 Ill.

Materialart: Digitale Medien

URL: http://dx.doi.org/10.1002/nme.1620340207

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Numerical study of shock-wave/boundary-layer interactions with bleed (1993)

Chyu, W. J. ; Hahn, T. O. ; Shih, T. I.-P.

In: Other Sources

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Publikationsdatum: 2011-08-24

Beschreibung: A numerical study was conducted to investigate how bleed through a two-dimensional slot affects shock-wave induced, boundary-layer separation on a flat plate. This study is based on the ensemble-averaged, compressible, Navier-Stokes equations closed by the Baldwin-Lomax, algebraic turbulence model. The algorithm used to obtain solutions was the implicit, partially split, two-factored scheme of Steger. This study examined the effects of the following parameters in controlling shock-wave induced flow separation: location of slot in relation to where the incident shock wave impinged on the boundary layer, size of slot in relation to the boundary-layer thickness, number of slots, spacings between slots, and strength of the incident shock wave. This study also showed the nature of the very complex flowfield about the slot or slots and how the plenum affects the bleed process. The results of this study are relevant to problems where bleed is used to control shock-wave induced, boundary-layer separation (e.g., inside jet engine inlets and wind tunnels).

Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER

Materialart: AIAA Journal (ISSN 0001-1452); 31; 5; p. 869-876.

Format: text

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Implicit treatment of diffusion terms in lower-upper algorithms (1993)

Steinthorsson, E. ; Chyu, W. J. ; Shih, T. I.-P.

In: Other Sources

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Publikationsdatum: 2011-08-24

Beschreibung: A method is presented which allows diffusion terms to be treated implicitly in the lower-upper (LU) algorithm (which is a commonly used method for solving 'compressible' Euler and Navier-Stokes equations) so that the algorithm's good stability properties will not be impaired. The new method generalizes the concept of LU factorization from that associated with the sign of eigenvalues to that associated with backward- and forward-difference operators without regard to eigenvalues. The method is verified in a turbulent boundary layer study.

Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER

Materialart: AIAA Journal (ISSN 0001-1452); 31; 4; p. 788-791.

Format: text

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4

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Approximate factorization with source terms (1991)

Shih, T. I.-P. ; Chyu, W. J.

In: Other Sources

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Publikationsdatum: 2011-08-19

Beschreibung: A comparative evaluation is made of three methodologies with a view to that which offers the best approximate factorization error. While two of these methods are found to lead to more efficient algorithms in cases where factors which do not contain source terms can be diagonalized, the third method used generates the lowest approximate factorization error. This method may be preferred when the norms of source terms are large, and transient solutions are of interest.

Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER

Materialart: AIAA Journal (ISSN 0001-1452); 29; 1759

Format: text

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Three-dimensional shock-wave/boundary-layer interactions with bleed through a circular hole (1992)

Rimlinger, M. J. ; Shih, T. I.-P. ; Chyu, W. J.

In: Other Sources

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Publikationsdatum: 2019-06-28

Beschreibung: Computations were performed to study three-dimensional (3-D), shock-wave/boundary-layer interactions on a flat plate in which fluid in the boundary layer was bled through a circular hole into a plenum to control shock-wave induced separation. Results are presented which show the details of the 3-D flowfield about the bleed hole and how bleed-hole placement relative to shock-wave impingement affect upstream, spanwise, and downstream influence lengths. This study revealed an underlying mechanisms by which bleed holes can affect shock-wave/boundary-layer interactions. This investigation is based on the ensemble-averaged, "full-compressible" Navier-Stokes equations closed by the Baldwin-Lomax turbulence model. Solutions to these equations were obtained by an implicit finite-volume method based on the partially-split, two-factored algorithm of Steger.

Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER

Materialart: AIAA PAPER 92-3084

Format: text

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Numerical studies of unsteady transonic flow over an oscillating airfoil (1984)

Chyu, W. J. ; Davis, S. S.

In: CASI

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Publikationsdatum: 2019-06-28

Beschreibung: A finite-difference solution to the Navier-Stokes equations combined with a time-varying grid-generation technique was used to compute unsteady transonic flow over an oscillating airfoil. These computations were compared with experimental data (obtained at Ames Research Center) which form part of the AGARD standard configuration for aeroelastic analysis. A variety of approximations to the full Navier-Stokes equations was used to determine the effect of frequency, shock-wave motion, flow separation, and airfoil geometry on unsteady pressures and overall air loads. Good agreement is shown between experiment and theory with the limiting factor being the lack of a reliable turbulence model for high-Reynolds-number, unsteady transonic flows.

Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER

Materialart: NASA-TM-86011 , A-9857 , NAS 1.15:86011

Format: application/pdf

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Überblick

7

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Three-dimensional shock-wave/boundary-layer interactions with bleed (1993)

Shih, T. I.-P. ; Rimlinger, M. J. ; Chyu, W. J.

In: Other Sources

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Publikationsdatum: 2019-07-13

Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER

Materialart: AIAA Journal (ISSN 0001-1452); 31; 10; p. 1819-1826.

Format: text

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