New Simulation Strategy for an Oscillating Cascade in Turbomachinery Using Immersed-Boundary Method-Reference-Cited by-同舟云学术

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New Simulation Strategy for an Oscillating Cascade in Turbomachinery Using Immersed-Boundary Method

Published:2009-03 Issue:2 Volume:25 Page:312-321
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Zhong Guohua¹,Sun Xiaofeng¹

Affiliation:

1. Beijing University of Aeronautics and Astronautics, 100083 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.35347

Reference34 articles.

1. Active control of aerofoil flutter

2. Effects of Wall Admittance Changes on Aeroelastic Stability of Turbomachines

3. Control of Blade Flutter by Smart-Casing Treatment

4. Acoustic Flutter Control of Three-Dimensional Transonic Rotor Flow

Cited by 15 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. Adaptive forcing distance in an immersed boundary method for internal flow simulation at high Reynolds numbers;Computers & Mathematics with Applications;2023-06

2. Application of immersed boundary method in turbomachines;Chinese Journal of Aeronautics;2023-05

3. Enhancement of Rotor Loading and Suppression of Stator Separation through Reduction of the Blade–Row Gap;International Journal of Turbomachinery, Propulsion and Power;2023-03-01

4. Simulating unsteady flows in a compressor using immersed boundary method with turbulent wall model;Aerospace Science and Technology;2021-08

5. Influence of non-uniform mean flow on acoustic scattering from complex geometries;Computers & Fluids;2018-02

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