AliAerospace/Rocket-Turbine-Studio
Design and geometry generation tool for rocket turbopump axial turbine rotor and vaned stator blades. Includes meanline analysis, various vortex laws, optimised blade shaping, rotor and stator blade generation, 3D geometry, and CAD export. Intended to be used alongside CFD for optimal blade shaping. Employs Sudhof's novel blade shaping methodology.
正在读取项目信息…