9:20 AM - 9:40 AM
[2022-a-06] Multi-Point Design Optimization of Fuel Injection Using Flexible Geometry for Scramjet-Powered Ascent Flight via Surrogate-Assisted Evolutionary Algorithms
Keywords:Scramjet Engine, Fuel Injector, Computational Fluid Dynamics, GPU, Space Transportation
In order to view paper PDF, please enter your "Full Paper viewing ID & Password" sent to you by email on or after 22 February.
» View Full Paper PDF