@inproceedings{oai:jaxa.repo.nii.ac.jp:00006136,
 author = {Lei, Zhong and Lei, Zhong},
 book = {宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2005論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005},
 month = {Feb},
 note = {In order to meet economic viability and environmental compatibility, the next generation supersonic transport (SST) is required to have sufficient low speed performance in take-off and landing situations. A high-lift system is desirable to enhance the lift as well as the lift-to-drag ratio. Wind tunnel test plays an important role in the design process of an aircraft. On the other hand, numerical simulation of high lift flews by solving the Reynolds-averaged Navier-Stokes (RANS) equations is now often used in analysis and design of high lift devices. It can provide details of flow structure and help designer to understand the physics of high lift flow. Accurate predictions of aerodynamic characteristics are required for the design of the high lift system. The objective of this study is to develop numerical simulation technology to predict aerodynamic performance of an SST configuration with high-lift devices, and give insight into details of flow field at low speed and high angles of attack., 資料番号: AA0049212003, レポート番号: JAXA-SP-05-017},
 pages = {23--28},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {低速における超音速機形態のRANSシミュレーション},
 volume = {JAXA-SP-05-017},
 year = {2006}
}