Computational fluid dynamics of multiphase flows in solid rocket motors

Material type: 文書・図像類

Author: 嶋田, 徹ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2006-03-31

Material Format: Digital

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Note (General)：: This booklet provides practical information on the computational fluid dynamics of the multiphase flows in solid rocket motors with descriptions of ma...

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Material Type: 文書・図像類
Title: Computational fluid dynamics of multiphase flows in solid rocket motors
Author/Editor: 嶋田, 徹
大門, 優
関野, 展弘
Shimada, Toru
Daimon, Yu
Sekino, Nobuhiro
Author Heading: 嶋田, 徹
大門, 優
関野, 展弘
Shimada, Toru
Daimon, Yu
Sekino, Nobuhiro
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2006-03-31
Publication Date (W3CDTF): 2006-03-31
Periodical title: 宇宙航空研究開発機構特別資料 = JAXA Special Publication
No. or year of volume/issue: JAXA-SP-05-035E
Volume: JAXA-SP-05-035E
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: eng
Subject Heading: 計算流体力学
固体推進剤ロケットエンジン
数値解析
数学モデル
オイラー・オイラー法
オイラー・ラグランジ法
オイラー・ハイブリッド法
固体燃料ロケットモータ
SRM
多相流
ガス-固体相互作用
化学平衡
燃焼
熱伝達
computational fluid dynamics
solid propellant rocket engine
numerical analysis
mathematical model
Eulerian-Eulerian method
Eulerian-Lagrangian method
Eulerian-hybrid method
solid rocket motor
multiphase flow
gas-solid interaction
chemical equilibrium
combustion
heat transfer
Target Audience: 一般
Note (General): This booklet provides practical information on the computational fluid dynamics of the multiphase flows in solid rocket motors with descriptions of mathematical modeling, simulation methods, computer codes, and many numerical experiments. Combustion flows of metallized composite propellants in solid rocket motors are multiphase flows consisting of particles and gas. In this booklet, descriptions are given concerning the mathematical modeling of the gas-particle interaction and its sensitivity on various parameters, simulation methods of gas-particle multiphase flows, such as, the Eulerian-Eulerian, the Eulerian-Lagrangian, and the Eulerian-hybrid methods, and the modeling method of combustion and breakup of particles, and so on. Computer programs, SPECS (Solid Propulsion Enhanced Code Series), coded along with these techniques are also introduced to the readers. Moreover, many examples of numerical experiments are provided on the verification of the mathematical modeling and numerical methods.
資料番号: AA0063153000
レポート番号: JAXA-SP-05-035E
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6093&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6093&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