Paper #84320

Paper information

Paper code: IAC-24,C4,7,3,x84320
Date: 2024-10-17
Time: 10:39
Order: 3
Room: Blue Hall 1
Title: Multi-Objective Design Optimization of Fuel Injection Using Flexible Geometry for Scramjet-Powered Ascent Flight via Surrogate-Assisted Evolutionary Algorithms
abstract: View PDF
Session: 7. Hypersonic Air-breathing and Combined Cycle Propulsion, and Hypersonic Vehicle
symposium: C4. IAF SPACE PROPULSION SYMPOSIUM
congress: IAC-24
Type of presentation: oral

Co-authors

Prof. Hideaki Ogawa, Kyushu University, Japan;

Dr. Masatoshi Kodera, Japan Aerospace Exploration Agency (JAXA), Japan;