Fuselage shape optimization of a wing-body configuration with nacelles

19th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2001, Pages

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

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b Project Development Department   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC DRAG; AERODYNAMICS; AIRFRAMES; COMPUTATIONAL FLUID DYNAMICS; FUSELAGES; STRUCTURAL FRAMES; SUPERSONIC AIRCRAFT;

AERODYNAMIC DESIGN TOOLS; AXI-SYMMETRICAL; DESIGN CONCEPT; DRAG MINIMIZATION; OPTIMIZATION DESIGN; OPTIMIZATION TECHNIQUES; STRONG INTERFERENCE; WING-BODY CONFIGURATIONS;

SHAPE OPTIMIZATION;

EID: 85067318093     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-2447     Document Type: Conference Paper

References (4)

1. Sakata, K., Supersonic Research Program in NAL, Japan, 1st International CFD Workshop for Super-Sonic Transport Design, pp. 1-4, 1998.
2. Makino, Y., Iwamiya, T., Numerical Simulation and Aerodynamic Design of an SST Configuration with Nacelles, AIAA paper 2000-0126, 2000.
3. Benek, J.A., Buning, P.G. and Steger, J.L., A 3-D Chimera Grid Embedding Technique, AIAA paper 85-1523, 1985.
4. Jameson, A., Optimum Aerodynamic Design Using CFD and Control Theory, AIAA paper 95-1729-CP, 1995.