ロケットエンジンターボポンプ用タービン段の翼形状最適化に関する研究

This study deals with an attempt to optimize blade profiles of 2-stage axial turbine section for a rocket engine turbopump, where the turbine section was originally designed by JAXA (Japan Aerospace Exploration Agency) in the project called DDT (Dynamic Design Team). An optimization based genetic al... View More