The propose of this project is to develop a three-dimensional, compressible Navier-Stokes solver for detailed study the flow inside transonic turbine and compressor's stator in the airplane turbomachinery.
The propose of this project is to develop a three-dimensional, compressible Navier-Stokes solver for detailed study the flow inside transonic turbine and compressor's stator in the airplane turbomachinery.
摘要本研究的目的在发展一系列飞机滑轮引擎之静子叶片的计算流体力学方法与程式，计算程式方面包括三维叶片格点的建立与黏性流程式开发及撰写等，程式发展完成后将进行一系列外形及气流条件计算模拟。