Aerodynamic design of unmanned and scaled supersonic experimental airplane in Japan

ECCOMAS 2004 - European Congress on Computational Methods in Applied Sciences and Engineering

Volumn , Issue , 2004, Pages

  Yoshida, Kenji ^a   Makino, Yoshikazu ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

Adjoint method; Arrow wing; Drag reduction; Inverse design method; Natural laminar flow

Indexed keywords

ADJOINT METHODS; AERODYNAMIC DESIGN TECHNOLOGY; FRICTION DRAG REDUCTIONS; INVERSE DESIGN METHODS; JAPAN AEROSPACE EXPLORATION AGENCY; NATURAL LAMINAR FLOWS; REDUCTION TECHNOLOGIES; SUPERSONIC WIND TUNNEL;

AIRCRAFT; COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL METHODS; DESIGN; DRAG REDUCTION; INTERFERENCE SUPPRESSION; JET ENGINES; LAMINAR FLOW; PLANFORMS; SPACE RESEARCH;

AERODYNAMICS;

EID: 84893456381     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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