| タイトル | Inlet-Compressor Analysis Performed Using Coupled Computational Fluid Dynamics Codes |
| 本文（外部サイト） | http://hdl.handle.net/2060/20050182031 |
| 著者（英） | Cole, Gary L.; Townsend, Scott; Suresh, Ambady |
| 著者所属（英） | DYNACS Engineering Co., Inc. |
| 発行日 | 1999-04-01 |
| 言語 | eng |
| 内容記述 | A thorough understanding of dynamic interactions between inlets and compressors is extremely important to the design and development of propulsion control systems, particularly for supersonic aircraft such as the High-Speed Civil Transport (HSCT). Computational fluid dynamics (CFD) codes are routinely used to analyze individual propulsion components. By coupling the appropriate CFD component codes, it is possible to investigate inlet-compressor interactions. The objectives of this work were to gain a better understanding of inlet-compressor interaction physics, formulate a more realistic compressor-face boundary condition for time-accurate CFD simulations of inlets, and to take a first step toward the CFD simulation of an entire engine by coupling multidimensional component codes. This work was conducted at the NASA Lewis Research Center by a team of civil servants and support service contractors as part of the High Performance Computing and Communications Program (HPCCP). |
| NASA分類 | Fluid Mechanics and Thermodynamics |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/86190 |
