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Adjoint-Based Multidisciplinary Design Optimization of Cooled Gas Turbine Blades

  • Published:2011-01-04 Issue: Volume: Page:
  • ISSN:
  • Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
  • language:
  • Short-container-title:

Author:

Mousavi Arash1,Nadarajah Siva1

Affiliation:

1. McGill University

Publisher

American Institute of Aeronautics and Astronautics

Reference39 articles.

1. Ruether, J., Jameson, A. Aerodynamic shape optimization of wing and wing-body configurations using CFD and control theory. AIAA paper 95-1729,

2. The harmonic adjoint approach to unsteady turbomachinery design

3. Adjoint Calculation of Sensitivities of Turbomachinery Objective Functions

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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. Study on continuous adjoint-based optimization method for internal cooling structures in turbine blades with conjugate heat transfer;Numerical Heat Transfer, Part B: Fundamentals;2023-11-28

3. Discrete adjoint for coupled conjugate heat transfer;Structural and Multidisciplinary Optimization;2023-04-17

4. Aerodynamic shape optimization of an electric aircraft motor surface heat exchanger with conjugate heat transfer constraint;International Journal of Heat and Mass Transfer;2022-06

5. Artificial intelligence aided design of film cooling scheme on turbine guide vane;Propulsion and Power Research;2020-12
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