Numerical simulation of flowfield around space plane traveling at Mach 10

Autor:	Manabe, Keiji, Sezaki, Shinji, Nishio, Masatomi
Jazyk:	japonština
Rok vydání:	2002
Předmět:	数値シミュレーション 極超音速流れの分布 宇宙機 numerical simulation hypersonic flow distribution finite element method マッハ数 aerospace plane 3次元モデル mach number three dimensional model 有限要素法
Zdroj:	航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2001論文集 = Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001. 53:257-261
ISSN:	0289-260X
Popis:	The numerical simulation around a space plane traveling at the speed of Mach 10 was carried out based on FEM (Finite Element Method). In this FEM formulation, stress (pressure) term is partially integrated in an element by applying the weighted residual method, and the hypersonic flowfield around a space plane model including shock wave can be calculated. three-dimensional simulations were conducted for the case of the angle of attack is 0 and 10 deg. The simulation results are compared with experimental results obtained by the electric discharge method, and good correlation between them was found. 資料番号: AA0032819044 レポート番号: NAL SP-53
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=jairo_______::a3bba89e87bf936946b8bb60aa4047c0 http://id.nii.ac.jp/1696/00038074/ Zobrazit plný text záznamu