Time-Linearized Navier-Stokes Analysis of Flutter in Multistage Turbomachines-Reference-Cited by-同舟云学术

Time-Linearized Navier-Stokes Analysis of Flutter in Multistage Turbomachines

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Ekici Kivanc¹,Voytovych Dmytro¹,Hall Kenneth¹

Affiliation:

1. Duke University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-836

Reference21 articles.

1. 3Silkowski, P. D., A Coupled Mode Method for Multistage Aeroelastic and Aeroacoustic Analysis of Turbomachinery, Ph.D. thesis,Duke University, Durham, NC27708,1996.

2. The Influence of Neighboring Blade Rows on the Unsteady Aerodynamic Response of Cascades

3. 1997 Best Paper Award—Structures and Dynamics Committee: A Coupled Mode Analysis of Unsteady Multistage Flows in Turbomachinery

Cited by 13 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. Review of Vibration Analysis and Structural Optimization Research for Rotating Blades;Journal of Marine Science and Application;2024-05-20

2. Efficient Acoustic Fan Flutter Analysis Using the Influence Coefficient Method and a Sliding Plane;Journal of Aerospace Engineering;2023-01

3. Experimental Study of the Vibration Phenomenon of Compressor Rotor Blade Induced by Inlet Probe Support;Journal of Thermal Science;2021-04-05

4. Effect of Front and Rear Rotor Stages on Aeroelasticity in Multi-Stage Environment;International Journal of Aeronautical and Space Sciences;2019-01-02

5. Influence of the Tip Clearance on a Compressor Blade Aerodynamic Damping;Journal of Propulsion and Power;2017-01