Adjoint formulation of a steady multistage turbomachinery interface using automatic differentiation

DOI10.1016/J.COMPFLUID.2018.09.015zbMath1410.76133OpenAlexW2890412445WikidataQ129208992 ScholiaQ129208992MaRDI QIDQ1625651

Sérgio S. Rodrigues, Andre C. Marta

Publication date: 29 November 2018

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2018.09.015

zbMATH Keywords

sensitivity analysisshape optimizationalgorithmic differentiationdiscrete adjointoperating conditionsendwall contouringmixing-plane

Mathematics Subject Classification ID

Numerical mathematical programming methods (65K05) General aerodynamics and subsonic flows (76G25) General theory of rotating fluids (76U05)

Uses Software

• PETSc
• TAPENADE

Cites Work

• Toward optimally seeded airflow on hypersonic vehicles using control theory
• Aerodynamic design via control theory
• Optimum aerodynamic design using the Navier-Stokes equations
• On the handling of turbulence equations in RANS adjoint solvers
• The Tapenade automatic differentiation tool
• Evaluating Derivatives
• A methodology for the development of discrete adjoint solvers using automatic differentiation tools
• On optimum design in fluid mechanics
• An introduction to the adjoint approach to design

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