Fuselage shape optimization of a wing-body configuration with nacelles

Journal of Aircraft

Volumn 40, Issue 2, 2003, Pages 297-302

  Makino, Yoshikazu ^a,c   Iwamiya, Toshiyuki ^a,d   Lei, Zhong ^b  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b Project Development Department   (Japan)

^c Next Generation Supersonic Transport   (Japan)

^d Compl Fluid Dynam Technol Center ^*  (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFRAMES; DRAG; FUSELAGES; OPTIMIZATION; WINGS;

FUSELAGE SHAPE OPTIMIZATION;

SUPERSONIC AERODYNAMICS;

EID: 0037362378     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.3093     Document Type: Article

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