Multidisciplinary Design Optimization for the Conceptual Design of Supersonic Civil Aircraft Based on Full-Carpet Sonic Boom/Aerodynamic Characteristics Employing Differential Evolution

Reducing the sonic boom intensity and increasing the cruise lift-to-drag ratio are pivotal technologies for the successful development of supersonic civil aircraft. To address the limitation that sonic boom research primarily focuses on characteristics directly beneath the flight track, a full-carpe...

Descripció completa

Dades bibliogràfiques

Autors principals:	Yuyu Duan, Chonweng Wan, Runze Li, Haixin Chen
Format:	Artigo
Idioma:	Inglês
Publicat:	MDPI AG 2026-01-01
Col·lecció:	Aerospace
Matèries:	supersonic civil aircraft sonic boom prediction multidisciplinary optimization full-carpet low-boom design conceptual design
Accés en línia:	https://www.mdpi.com/2226-4310/13/1/96
Etiquetes:	Afegir etiqueta Sense etiquetes, Sigues el primer a etiquetar aquest registre!