並列タイトル等Aerodynamic Simulation of Flows About a Space-Plane III
タイトル（掲載誌）航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-10
一般注記Three dimensional flowfields about a winged space vehicle at supersonic speed has been numerically simulated using Navier-Stokes equations. The present model of the vehicle is under research at the National Aerospace Laboratory as a candidate of Japanese future aerospace vehicle. Our interest is concentrated on the comprehension of the effect of the tail wing or the shape of the vehicle. So, two different simulations has been conducted; One is for the flowfields about a whole configuration model (WBT Model) and the other is about a wing-body combination model (WB Model). The vortical flow phenomena due to high angle of attack are so complicated that a more and more careful consideration would be necessary. The numerical results show the difference clearly between those two flowfields. The aerodynamic forces and coefficients computed from the simulation results are in good agreement with experimental data.
資料番号: NALSP0010045
レポート番号: NAL SP-10
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
提供元機関・データベース宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ