Surrogate Based Shape Optimization of a Low Boom Fuselage Wing Configuration
AIAA Aviation 2019 Forum
2019-01-01
Conference paper
Electronic Resource
English
AIAA-2019-3489: Surrogate Based Shape Optimization of a Low Boom Fuselage Wing Configuration
British Library Conference Proceedings | 2019
|British Library Conference Proceedings | 2016
|FUSELAGE SHAPE OPTIMIZATION AIMED AT WING-FUSELAGE CONFIGURATION DRAG REDUCTION AT SUPERSONIC SPEEDS
DOAJ | 2017
|