Two-dimensional high-lift aerodynamic optimization using the continuous adjoint method

8th Symposium on Multidisciplinary Analysis and Optimization

Volumn , Issue , 2000, Pages

  Kim, Sangho ^a   Alonso, Juan J ^a,b   Jameson, Antony ^a,b  

^a STANFORD UNIVERSITY   (United States)

^b Department of Aeronautics and Astronautics ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; ANGLE OF ATTACK; DRAG; FINITE DIFFERENCE METHOD; INVERSE PROBLEMS; LIFT; LIFT DRAG RATIO; MESSAGE PASSING; REYNOLDS NUMBER; TURBULENCE MODELS;

AERODYNAMIC OPTIMIZATION; CONFIGURATION DESIGN METHODS; CONTINUOUS ADJOINT METHODS; DESIGN AND OPTIMIZATION; MESSAGE PASSING INTERFACE; REYNOLDS AVERAGED NAVIER STOKES (RANS)EQUATIONS; REYNOLDS-AVERAGED NAVIER-STOKES FLOW SOLVERS; SPALART-ALLMARAS TURBULENCE MODEL;

NAVIER STOKES EQUATIONS;

EID: 85085402971     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-4741     Document Type: Conference Paper

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