有限面積法による二次元翼列まわりの非粘性圧縮流の数値計算

Material type: 文書・図像類

Author: 福田, 正大ほか

Publisher: 航空宇宙技術研究所

Publication date: 1982-05

Material Format: Digital

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Note (General)：: The steady inviscid compressible flow through the two-dimensional cascade is computed by the Method of Time-Dependent Finite Area with hexagonal integ...

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Material Type: 文書・図像類
Title: 有限面積法による二次元翼列まわりの非粘性圧縮流の数値計算
Author/Editor: 福田, 正大
西村, 英明
田村, 敦宏
FUKUDA, Masahiro
NISHIMURA, Hideaki
TAMURA, Atsuhiro
Author Heading: 福田, 正大
西村, 英明
田村, 敦宏
FUKUDA, Masahiro
NISHIMURA, Hideaki
TAMURA, Atsuhiro
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1982-05
Publication Date (W3CDTF): 1982-05
Alternative Title: Numerical Simulation of Inviscid Compressible Flow through Two-Dimensional Cascade by Finite Area Method
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-709
No. or year of volume/issue: 709
Volume: 709
Pages: 16-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Target Audience: 一般
Note (General): The steady inviscid compressible flow through the two-dimensional cascade is computed by the Method of Time-Dependent Finite Area with hexagonal integral domain. Three different equation systems are considered which are physically equivalent under two assumptions: i) steady state, ii)subsonic or exsting weak shock flow field. The basic system is composed of the continuity equation, the Eular equation and the energy equation. Their differences during numerical behavior approaching the steady state have been examined through computations. To prevent the pressure or the density from becoming negative, the spatial averaging for smoothing was used, which appears to have some artificial viscocity and damping factor for time-dependent computations. In the steady state computed airfoil pressure distributions have shown good agreement with experimental measurements and there have been few differences among the three equation systems.
資料番号: NALTR0709000
レポート番号: NAL TR-709
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44966&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44966&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