3-D Aerodynamic Shape Design Using Hessians Based on Incomplete Sensitivities

DOI10.1080/10618560008940718zbMath1033.76051OpenAlexW2071393204MaRDI QIDQ2744219

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Publication date: 28 March 2004

Published in: International Journal of Computational Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/10618560008940718

zbMATH Keywords

optimizationautomatic differentiationBroyden-Fletcher-Goldfarb-Shannon methodapproximate sensitivitiessupersonic wingstransonic wingsunstructured flow solver

Mathematics Subject Classification ID

Transonic flows (76H05) Finite volume methods applied to problems in fluid mechanics (76M12) Supersonic flows (76J20) Flow control and optimization for compressible fluids and gas dynamics (76N25)

Cites Work

• Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methods
• A comparison of optimization-based approaches for a model computational aerodynamics design problem
• Progressive optimization of inverse fluid dynamic design problems
• Using Complex Variables to Estimate Derivatives of Real Functions
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