@inproceedings{oai:jaxa.repo.nii.ac.jp:00004714,
 author = {丸山, 祐一 and Maruyama, Yuichi},
 book = {宇宙航空研究開発機構特別資料: 第42回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2010 論文集, JAXA Special Publication: Proceedings of 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010},
 month = {Feb},
 note = {第42回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2010 (2010年6月24日-25日. 米子コンベンションセンター BiG SHiP), 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010 (June 24-25,  2010. Yonago Convention Center BiG SHiP), Yonago, Tottori Japan, In STOL, it is critical to maintain lifting power stably at low speed. For this purpose, jet from the engine flows along the wing surface to create a large uptrend centrifugal force which yields an additional uplift force on the wing. In this research, numerical calculation using the Large Eddy Simulation method is performed to find out about this special characteristic of jet under the influence of inertial forces and turbulence. It is seen that the secondary flow appears within the jet and its vicinity. Pressure gradient normal to the wing surface, which creates the lift force, is increased by the addition of jet. The value of the pressure gradient depends on the radius of curvature of the wing surface and the ratio of the flow velocity within the jet to that outside, while the increase rate depends on the latter alone. It is also observed that the movement direction of the jet center is slightly dislocated from the centrifugal force if the jet is swirling. The distribution of the chordwise component of Coriolis force is asymmetric within the jet, and it is estimated that the fluid speeds up in one half of the jet and slows down in the other half, which causes the jet center to move laterally., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064967007, レポート番号: JAXA-SP-10-012},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {慣性力影響下での旋回噴流の挙動についての研究},
 volume = {JAXA-SP-10-012},
 year = {2011}
}