[A-2] Air-breathing Engine 1

[2022-a-06] Multi-Point Design Optimization of Fuel Injection Using Flexible Geometry for Scramjet-Powered Ascent Flight via Surrogate-Assisted Evolutionary Algorithms

*Mehmet Aksay¹, Shuvayan Brahmachary¹, Kento Akiyama¹, Hideaki Ogawa¹ (1. Kyushu University, Department of Aeronautics and Astronautics)

キーワード：Scramjet Engine, Fuel Injector, Computational Fluid Dynamics, GPU, Space Transportation