MULTI-POINT DESIGN OPTIMIZA TION OF BUSEMANN BASED INTAKES FOR SCRAMJET-POWERED ASCENT FLIGHT VIA SURROGATE-ASSISTED EVOLUTIONARY
AIAA SciTech Forum and Exposition ; 2021 ; Online
2021
Aufsatz (Konferenz)
Englisch
BKL: | 55.50 Luftfahrzeugtechnik |