| タイトル | Computational Analysis of the Effect of Porosity on Shock Cell Strength at Cruise |
| 本文（外部サイト） | http://hdl.handle.net/2060/20060023987 |
| 著者（英） | Hunter, Craig A.; Abdol-Hamid, Khaled S.; Pao, S. Paul; Elmiligui, Alaa A.; Massey, Steven J. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2006-05-01 |
| 言語 | eng |
| 内容記述 | A computational flow field analysis is presented of the effect of core cowl porosity on shock cell strength for a modern separate flow nozzle at cruise conditions. The goal of this study was to identify the primary physical mechanisms by which the application of porosity can reduce shock cell strength and hence the broadband shock associated noise. The flow is simulated by solving the asymptotically steady, compressible, Reynoldsaveraged Navier-Stokes equations on a structured grid using an implicit, up-wind, flux-difference splitting finite volume scheme. The standard two-equation k - epsilon turbulence model with a linear stress representation is used with the addition of a eddy viscosity dependence on total temperature gradient normalized by local turbulence length scale. Specific issues addressed in this study were the optimal area required to weaken a shock impinging on the core cowl surface and the optimal level of porosity and placement of porous areas for reduction of the overall shock cell strength downstream. Two configurations of porosity were found to reduce downstream shock strength by approximately 50%. |
| NASA分類 | Fluid Mechanics and Thermodynamics |
| レポートNO | AIAA Paper 2006-2468 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
