The application of MDO technologies to the design of a high performance small jet aircraft - Lessons learned and some practical concerns

35th AIAA Fluid Dynamics Conference and Exhibit

Volumn , Issue , 2005, Pages

  Takenaka, Keizo ^a   Obayashi, Shigeru ^b   Nakahashi, Kazuhiro ^b   Matsushima, Kisa ^b  

^a MITSUBISHI HEAVY INDUSTRIES LTD   (Japan)

^b TOHOKU UNIVERSITY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC OPTIMIZATION; HIGH-LIFT DEVICES; MAXIMUM TAKEOFF WEIGHTS; MULTI-DISCIPLINARY OPTIMIZATIONS; NONDOMINATED SOLUTIONS; OBJECTIVE FUNCTIONS; OPTIMIZED SOLUTIONS; TECHNICAL FEATURES;

AEROELASTICITY; AIRCRAFT MANUFACTURE; DESIGN; FLUID DYNAMICS; JET AIRCRAFT; OPTIMIZATION;

AERODYNAMICS;

EID: 84884945663     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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