Paper information

Paper code

IAC-21,C4,7,6,x64770

Date

2021-10-28

Time

11:45

Order

1006

Room

Ajman D

Title

Multi-Point 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-21

Type of presentation

oral

Main author

Mr. Mehmet AKSAY, Kyushu University, Japan

Co-authors

Dr. Shuvayan Brahmachary, Kyushu University, Japan;

Prof. Hideaki Ogawa, Kyushu University, Japan;

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

Dr. Sadatake Tomioka, Japan Aerospace Exploration Agency (JAXA), Japan;