CFD analysis results on NEXST-1
| Autor: | Jeong, Shinkyu, Misaka, Takashi |
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| Jazyk: | angličtina |
| Rok vydání: | 2007 |
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| Zdroj: | 宇宙航空研究開発機構特別資料 = JAXA Special Publication: Proceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop). :672-680 |
| ISSN: | 1349-113X |
| Popis: | SST-CFDワークショップ.次世代超音速機の数値シミュレーション利用技術に関する国際ワークショップ: Toward the Future form NEXST-1 Flight Trial 宇宙航空研究開発機構 20061012-20061013 東京 日本 SST-CFD Workshop. International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport: Toward the Future form NEXST-1 Flight Trial Japan Aerospace Exploration Agency 20061012-20061013 Tokyo Japan In this study, flow computations were performed on the NEXST-1 (National EXperiment Supersonic Transport-1) with unstructured mesh solver. Two different meshes and two different turbulence models were used. The computational results were compared with NEXST-1's flight data. As a whole, the computational result showed a good agreement with flight data, except the pressure distribution on the lower surface in alpha-sweep cases. 資料番号: AA0063609074 レポート番号: JAXA-SP-06-029E |
| Databáze: | OpenAIRE |
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