タイトル | Navier-Stokes solutions for flows related to store separation |
本文(外部サイト) | http://hdl.handle.net/2060/19910001548 |
著者(英) | Baysal, Oktay; Stallings, Robert L., Jr.; Plentovich, Elizabeth B. |
著者所属(英) | NASA Langley Research Center |
発行日 | 1989-09-01 |
言語 | eng |
内容記述 | The objective is developing CFD capabilities to obtain solutions for viscous flows about generic configurations of internally and externally carried stores. The emphasis is placed on the supersonic flow regime with extensions being made to the transonic regime. The project is broken into four steps: (1) Cavity flows for internal carriage configurations; (2) High angle of attack flows, which may be experienced during the separation of the stores: (3) Flows about a body near a flat plate for external carriage configurations; and (4) Flows about a body inside or in the proximity of a cavity. Three-dimensional unsteady cavity flow solutions are obtained by an explicit, MacCormack algorithm, EMCAV3, for open, close, and transitional cavities. High angle of attack flows past cylinders are solved by an implicit, upwind algorithm. All the results compare favorably with the experimental data. For flows about multiple body configurations, the Chimera embedding scheme is modified for finite-volume and multigrid algorithms, MaGGiE. Then a finite volume, implicit, upwind, multigrid Navier-Stokes solver which uses on overlapped/embedded and zonal grids, VUMXZ3, is developed from the CFL3D code. Supersonic flows past a cylinder near a flat plate are computed using this code. The results are compared with the experimental data. Currently the VUMXZ3 code is being modified to accomplish step 4 of this project. Wind tunnel experiments are also being conducted for validation purposes. |
NASA分類 | AERODYNAMICS |
レポートNO | 91N10861 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/135664 |
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