| タイトル | Supersonic Combustion Research at NASA |
| 本文（外部サイト） | http://hdl.handle.net/2060/20080013391 |
| 著者（英） | Drummond, J. P.; Danehy, Paul M.; Gaffney, Richard L., Jr.; Cutler, Andrew D.; Bivolaru, Daniel; Tedder, Sarah A. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2007-10-24 |
| 言語 | eng |
| 内容記述 | This paper discusses the progress of work to model high-speed supersonic reacting flow. The purpose of the work is to improve the state of the art of CFD capabilities for predicting the flow in high-speed propulsion systems, particularly combustor flowpaths. The program has several components including the development of advanced algorithms and models for simulating engine flowpaths as well as a fundamental experimental and diagnostic development effort to support the formulation and validation of the mathematical models. The paper will provide details of current work on experiments that will provide data for the modeling efforts along with the associated nonintrusive diagnostics used to collect the data from the experimental flowfield. Simulation of a recent experiment to partially validate the accuracy of a combustion code is also described. |
| NASA分類 | Aircraft Propulsion and Power |
| 権利 | Copyright, Distribution as joint owner in the copyright |
