Design of a low-boom supersonic business jet using evolutionary algorithms and an adaptive unstructured mesh method

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 4, Issue , 2004, Pages 2692-2706

  Choi, Seongim ^a   Alonso, Juan J ^a   Chung, Hyoung S ^b  

^a STANFORD UNIVERSITY   (United States)

^b Korean Air Force Academy   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE UNSTRUCTURED MESH METHOD; AERODYNAMIC SHAPE OPTIMIZATION; AIRCRAFT SURFACE; INITIAL PRESSURE JUMP;

ADAPTIVE CONTROL SYSTEMS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER AIDED DESIGN; CONSTRAINT THEORY; COSTS; EVOLUTIONARY ALGORITHMS; JET AIRCRAFT; NAVIER STOKES EQUATIONS; OPTIMAL SYSTEMS; OPTIMIZATION; PARETO PRINCIPLE; PROBLEM SOLVING;

SUPERSONIC AIRCRAFT;

EID: 16244418354     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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