Recent advancements in turbomachinery forced response analyses-Reference-Cited by-同舟云学术

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Recent advancements in turbomachinery forced response analyses

Published:1992-01-06 Issue: Volume: Page:
ISSN:
Container-title:30th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

KIELB ROBERT¹,CHIANG HSIAO-WEI¹

Affiliation:

1. GE Aircraft Engines, Cincinnati, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-12

Reference85 articles.

1. Vibration Amplitudes of Mistuned Blades

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. Hybrid LES/RANS Simulations of Compressible Flow in a Linear Cascade of Flat Blade Profiles;Journal of Thermal Science;2024-07-02

2. Numerical Investigation of Classic Flutter Mechanism Under Circumferentially Non-Uniform Inlet Condition;Journal of Turbomachinery;2024-01-29

3. Flutter in a simplified blade cascade: Limits of the quasi-steady approximation;Journal of Fluids and Structures;2023-07

4. Forced Response Analysis of an Embedded Compressor Rotor Induced by Stator Disturbances and Rotor–Stator Interactions;Aerospace;2023-04-25

5. Aerodynamic and Aeroelastic Effects of Design-Based Geometry Variations on a Low-Pressure Compressor;International Journal of Turbomachinery, Propulsion and Power;2020-09-24

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