@techreport{oai:jaxa.repo.nii.ac.jp:00041216,
 author = {山本, 武 and 田丸, 卓 and Yamamoto, Takeshi and Tamaru, Takashi},
 month = {Apr},
 note = {ラムジェットエンジン燃焼器用保炎器として、耐熱性の観点から燃料噴出型保炎器が有望と考えられる。その2次元化模型まわりの水素の燃焼を伴う流れの数値シミュレーションコードを開発した。解法としてSIMPLER法、乱流モデルとして明・笠木のk-ε2方程式モデル、燃焼モデルとして渦消散モデルを用いた。このCFD(計算流体力学)コードの詳細といくつかの典型的な計算結果を示す。, In the National Aerospace Laboratory, research work on a hydrogen-fueled ramjet engine for the spaceplane is being carried out. As a part of this research, a bluff-body type flame holder with fuel injection was tested at atmospheric conditions and prospective results were obtained for the engine. However, the capability of the experimental facility was limited, and it was difficult to investigate the engine performance over a wide operating range. So a two-dimensional CFD (Computational Fluid Dynamics) code was developed to simulate engine performance over a wide operating range. The code is based on the SIMPLER algorithm, and the power law scheme is used for the discretization of the governing equations. Turbulence is simulated by Myong-Kasagi's low Reynolds number type kappa-epsilon model. Magnussen's eddy dissipation concept is used to simulate the combustion. In this report, details of the CFD code and some typical results of the numerical simulation are described., 資料番号: AA0004246000, レポート番号: NAL TR-1233},
 title = {燃料噴出型保炎器周りの流れに関する数値シミュレーションコードの開発},
 year = {1994}
}