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Interpretation of Adjoint Solutions for Turbomachinery Flows

  • Published:2013-07 Issue:7 Volume:51 Page:1733-1744
  • ISSN:0001-1452
  • Container-title:AIAA Journal
  • language:en
  • Short-container-title:AIAA Journal

Author:

Marta Andre C.1,Shankaran Sriram2,Wang Qiqi3,Venugopal Prem4

Affiliation:

1. Center for Aerospace Science and Technology, Instituto Superior Técnico, Lisbon 1049, Portugal

2. Fluid Mechanics Lab., Global Research Center, General Electric, Niskayuna, New York 12309

3. Department of Aeronautics, Massachusetts Institute of Technology, Cambridge, Masachussetts 02139

4. Turbomachinery Aerodynamics Lab, Global Research Center, General Electric, Niskayuna, New York 12309

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference30 articles.

1. Numerical Optimization

2. GriewankA., Evaluating Derivatives, Society for Industrial and Applied Mathematics, Philadelphia, PA, 2000, pp. 13–118.

3. On optimum design in fluid mechanics

4. Aerodynamic design via control theory

5. Optimum Aerodynamic Design Using the Navier-Stokes Equations

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1. A review on aerodynamic optimization of turbomachinery using adjoint method;Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science;2024-01-23

2. Analytic adjoint solutions for the 2-D incompressible Euler equations using the Green's function approach;Journal of Fluid Mechanics;2022-06-13

3. Multi-Objective Optimization of Cascade Blade Profile Based on Reinforcement Learning;Applied Sciences;2020-12-24

4. Watch Your Adjoints! Lack of Mesh Convergence in Inviscid Adjoint Solutions;AIAA Journal;2019-09

5. Adjoint-based shape sensitivity of multi-row turbomachinery;Structural and Multidisciplinary Optimization;2019-08-31
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