Aerodynamic design using the truncated Newton algorithm and the continuous adjoint approach

DOI10.1002/fld.2530zbMath1452.76209OpenAlexW2122071276MaRDI QIDQ2900461

Kyriakos C. Giannakoglou, Dimitrios I. Papadimitriou

Publication date: 23 July 2012

Published in: International Journal for Numerical Methods in Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/fld.2530

zbMATH Keywords

Euler equationsconjugate gradient methodshape optimizationdirect differentiationHessian matrixsecond-order sensitivity derivative

Mathematics Subject Classification ID

Numerical optimization and variational techniques (65K10) Flow control and optimization for compressible fluids and gas dynamics (76N25) Basic methods in fluid mechanics (76M99)

Related Items (3)

Approximate Hessian for accelerated convergence of aerodynamic shape optimization problems in an adjoint-based framework ⋮ Pfosm: an efficient algorithm for aerodynamic robust design based on continuous adjoint and matrix-vector products ⋮ Adjoint-assisted Pareto front tracing in aerodynamic and conjugate heat transfer shape optimization

Uses Software

• tn

Cites Work

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• A Numerical Study of the Limited Memory BFGS Method and the Truncated-Newton Method for Large Scale Optimization
• Numerical Optimization
• Numerical methods for second‐order shape sensitivity analysis with applications to heat conduction problems
• A Preconditioning Method for Shape Optimization Governed by the Euler Equations
• On optimum design in fluid mechanics

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