@inproceedings{oai:jaxa.repo.nii.ac.jp:00003500,
 author = {森田, 直人 and 土屋, 武司 and Morita, Naoto and Tsuchiya, Takeshi},
 book = {宇宙航空研究開発機構特別資料: 第48回流体力学講演会/第34回航空宇宙数値シミュレーション技術シンポジウム論文集, JAXA Special Publication: Proceedings of the 48th Fluid Dynamics Conference / the 34th Aerospace Numerical Simulation Symposium},
 month = {Dec},
 note = {第48回流体力学講演会/第34回航空宇宙数値シミュレーション技術シンポジウム (2016年7月6日-8日. 金沢歌劇座), 金沢市, 石川, 48th Fluid Dynamics Conference /the 34th Aerospace Numerical Simulation Symposium (July 6-8, 2016. The Kanazawa Theatre), Kanazawa, Ishikawa, Japan, For the realization of the space plane, the high accuracy of aerodynamic estimation and system analyses are needed. In our past studies, we have obtained an optimal configuration of waverider-winged spaceplanes by using simultaneous trajectory and design optimization. As a further research of the result, we conducted CFD analyses on the obtained spaceplane. Our studies compared results of FaSTAR, which is developed by Japan Aerospace Exploration Agency, and panel methods. We used PANAIR which is panel method with high accuracy and HYPER which is solver of modified newtonian as the panel methods. When we compared between the results of the CFD and the panel methods, the CL and CD values are similar to the both results. However in almost all of the mach numbers, the panel methods estimated smaller Cm values than the CFD code. This is because panel method cannot consider interference of shock wave between body and wing.  In addition, the effectiveness of V-tail was estimated in smaller value than CFD's results. Then, we should pay attention to the interference between wing and body when we consider problems using panel methods or establish more reliably combinations of panel methods and CFDs to do more accurate aerodynamic analyses about the space planes' optimization., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1630031025, レポート番号: JAXA-SP-16-007},
 pages = {183--188},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {膨張領域を持つwaveriderの数値解析および簡易空力評価法との比較},
 volume = {JAXA-SP-16-007},
 year = {2016}
}