Computation of the Hessian matrix in aerodynamic inverse design using continuous adjoint formulations

Computers and Fluids

Volumn 37, Issue 8, 2008, Pages 1029-1039

  Papadimitriou, D I ^a   Giannakoglou, K C ^a  

^a NATIONAL TECHNICAL UNIVERSITY OF ATHENS   (Greece)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE APPLICATIONS; AIR; AIRFOILS; ARCHITECTURAL DESIGN; COMPUTATIONAL METHODS; DIFFERENTIATION (CALCULUS); EQUIVALENCE CLASSES; FUNCTION EVALUATION; FUNCTIONS; GAS DYNAMICS; GRADIENT METHODS; INVERSE PROBLEMS; MATRIX ALGEBRA; NEWTON-RAPHSON METHOD; OPTICAL DEVICES; OPTIMAL CONTROL SYSTEMS; OPTIMIZATION; VISCOUS FLOW;

ADJOINT; AERODYNAMIC DESIGNS; CASCADE (CO); DEGREES OF FREEDOM; DIRECT DIFFERENTIATION; DIRECT DIFFERENTIATION METHOD (DDM); ELSEVIER (CO); FLOW EQUATIONS; FLOW SOLUTIONS; HESSIAN MATRICES; INVERSE DESIGN (ID); INVISCID FLOWS; NEWTON METHODS; OBJECTIVE FUNCTION (OF); OPTIMIZATION TOOLS; PARALLELIZATION; SECOND-ORDER DERIVATIVES; SENSITIVITY DERIVATIVES; SINGLE-OBJECTIVE OPTIMIZATIONS; SOLID BOUNDARIES;

NUMERICAL METHODS;

EID: 45449111386     PISSN: 00457930     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compfluid.2007.11.001     Document Type: Article

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