The Space race has begun again, driven by demand for low Earth orbit 5G satellite constellations, Space Tourism, Defense systems, and even the colonization of Mars. And with it, the intense pressure to innovate faster. This webinar will highlight the integration and acceleration of many engineering disciplines and tools, from mission and systems engineering to detailed design and analysis of rocket propulsion components, featuring technology from Ansys, ADT, and Flownex.
This paper describes the new method of full 3D design for axial turbine nozzles and blades by applying the 3D inverse design method in which the blade geometry can be determined by specified distributions of circulation and blade blade thickness.
In this paper, a methodology is presented based on coupling a 3D inverse design method together with Design of Experiments, Response Surface modeling and Multi-objective Genetic algorithms in order to improve the efficiency and tonal noise from high rpm cooling fans.
A fully three-dimensional compressible inverse design method for the design of radial and mixed flow turbomachines in described in this paper. Two approaches are presented for solving the compressible flow problem: approximate and exact approaches.