| Hayder, M. E. and Turkel, E. "High Order Accurate Solutions of Viscous Problems". 31st AIAA Aerospace Sciences Conference, AIAA 93-3074, July 1993. |
.... [168] in which they extend the results of [167] for the case of realistic (nonideal) thermodynamic relations and reacting flows; work by Grinstein [169] in which the local ABC s for the boundaries that intersect the regions of turbulent mixing layers are analyzed; work by Hayder and Turkel [170,171], in which the authors experimentally study the performance of different local boundary conditions, including those of [72] 91] and [116] several types of radiation boundary conditions (purely inviscid and those that take into account some viscous corrections) as well as a sponge layer (see ....
....L. Zhao and Cangellaris [183] considerations. In this paper, we do not concentrate on describing the boundary treatment techniques based on absorbing layers. We only mention some work done in this area by different authors. Besides the previously discussed work by Clement [96] Hayder and Turkel [170], Berenger [179, 180] Abarbanel and Gottlieb [181, 184] Petropoulos [182] and L. Zhao and Cangellaris [183] we additionally mention work by Israeli and Orszag [185] R. Kosloff and D. Kosloff [186] Karni [187] Hu [188] Collino [189] Jin and Chew [190] Kantartzis and Tsiboukis [191] ....
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M. E. Hayder and E. Turkel, High Order Accurate Solutions of Viscous Problems, AIAA Paper No. 93-3074, 24th AIAA Fluid Dynamics Conference, Orlando, Florida, 1993.
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Hayder, M. E. and Turkel, E. "High Order Accurate Solutions of Viscous Problems". 31st AIAA Aerospace Sciences Conference, AIAA 93-3074, July 1993.
....equations. For supersonic flows, all the R i at the outflow boundary can be calculated from the Navier Stokes equations or by extrapolation of all the characteristic variables from the interior. This framework of outflow boundary condition implementation is discussed by Hayder and Turkel [10]. Further discussions of our numerical model including other boundary treatments are given in Hayder et al. 11] and Mankbadi et al. 12] In this study, we consider a jet with the mean inflow profile U r = U1 (U c Gamma U1 )g r T r = T c (T 1 Gamma T c )g r fl Gamma 1 2 M 2 c (1 ....
Hayder, M. E. and Turkel, E. "High Order Accurate Solutions of Viscous Problems". 31st AIAA Aerospace Sciences Conference, AIAA 93-3074, January 1993.
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