Numerical Simulation of Hypersonic Flow Around a Space Plane II Application to High Angles of Attack Flow

Material type: 文書・図像類

Author: 山本, 行光ほか

Publisher: 航空宇宙技術研究所

Publication date: 1989-02

Material Format: Digital

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Note (General)：: 流束分離TVD風上差分法をスペース・プレーンまわりの超音速流の解析に適用した。今回の解析では主翼後方のWake領域を含め,大仰角における計算を可能とした。基礎方程式は有限体積表示の薄層近似ナビエ・ストークス方程式で,解法はIAF(Implicit Approximate Factorization)...

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Material Type: 文書・図像類
Title: Numerical Simulation of Hypersonic Flow Around a Space Plane II Application to High Angles of Attack Flow
Author/Editor: 山本, 行光
YAMAMOTO, Yukimitsu
Author Heading: 山本, 行光
YAMAMOTO, Yukimitsu
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1989-02
Publication Date (W3CDTF): 1989-02
Periodical title: Technical Report of National Aerospace Laboratory TR-1011T
No. or year of volume/issue: 1011T
Volume: 1011T
Pages: 20-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: eng
Target Audience: 一般
Note (General): 流束分離TVD風上差分法をスペース・プレーンまわりの超音速流の解析に適用した。今回の解析では主翼後方のWake領域を含め,大仰角における計算を可能とした。基礎方程式は有限体積表示の薄層近似ナビエ・ストークス方程式で,解法はIAF(Implicit Approximate Factorization)法である。数値計算はマッハ数7.0, レイノルズ数4.4×10(exp 6)で迎角は10度間隔で0度から50度までのケースについて行った。計算結果は当初の超音速風洞で行われた実験結果と比較し,空力特性について良好な一致が得られた。
a Flux-split upwind TVD scheme has been applied to the hypersonic flow around a space plane proposed by National Aerospace laboratory (NAL). Thin-layer Navier-Stokes equations in a finite volume formulation are solved by using an implicit approximately factored ADI algorithm. Numerical computations are performed for a Mach number of 7.0 and Reynolds number of 4.4×10(exp 6) at angles of attack up to 50 degrees. Numerical results are compared with experimental data obtained from the hypersonic wind tunnel tests st NAL. Through these comparisons, it is demonstrated that the present TVD Navier-Stokes code has excellent capabilities for evaluating total aerodynamic performance and investigating aerodynamic heating, which are of great significance in the design of a space plane configuration.
資料番号: NALTR1011000
レポート番号: NAL TR-1011T
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45270&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45270&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
Data Provider (Database): 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）
https://irdb.nii.ac.jp
Original Data Provider (Database): 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