Hydrodynamic shape optimization of propulsor configurations using continuous adjoint approach-Reference-Cited by-同舟云学术

Hydrodynamic shape optimization of propulsor configurations using continuous adjoint approach

Published:2001-06-11 Issue: Volume: Page:
ISSN:
Container-title:15th AIAA Computational Fluid Dynamics Conference
language:
Short-container-title:

Author:

Dreyer James¹,Martinelli Luigi²

Affiliation:

1. Pennsylvania State Univ., University Park

2. Princeton Univ., NJ

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-2580

Reference34 articles.

1. [I] Busby, J.A. "Unsteady Three-Dimensional Incompressible Flow Interaction in Multiple-Blade-Row Turbomachinery," Ph.D. Dissertation,Mississippi State University, 1997.

2. Dreyer, J.J., Zierke, W.C. "Solution of the Average Passage Equations for the Incompressible Flow Through Multiple-Blade-Row Turbomachinery," ARL Penn State Technical Report No. 94-05, Applied Research Laboratory, The Pennsylvania State University, Feb. 1994.

3. Aerodynamic design via control theory

4. Automatic aerodynamic optimization on distributed memory architectures

Cited by 9 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Aerodynamic adjoint optimization of turbomachinery with direct control on blade design parameters;Chinese Journal of Aeronautics;2023-11

2. Adjoint optimization of a multi-row transonic compressor based on an extended free-form method;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2023-06-09

3. Multi-Objective Optimization of a Transonic Compressor Rotor by Using an Adjoint Method;AIAA Journal;2015-03

4. Turbine Blade Row Optimization Through Endwall Contouring by an Adjoint Method;Journal of Propulsion and Power;2015-03

5. Entropy minimization in turbine cascade using continuous adjoint formulation;Engineering Optimization;2015-01-22