Separation of Wake and Potential Field Excitations in an Embedded Compressor Rotor: Impact of Wave Reflections and mistuning on Forced Response-Reference-Cited by-同舟云学术

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Separation of Wake and Potential Field Excitations in an Embedded Compressor Rotor: Impact of Wave Reflections and mistuning on Forced Response

Published:2021-01-04 Issue: Volume: Page:
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Container-title:AIAA Scitech 2021 Forum
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Author:

Hegde Shreyas¹,Zori Laith²,Campregher Rubens²,Kielb Robert¹

Affiliation:

1. Duke University

2. ANSYS, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Reference40 articles.

1. Experimental Characterization of Tip Leakage Flow Trajectories in a Multistage Compressor

2. Mistuned Forced Response Predictions of an Embedded Rotor in a Multistage Compressor

3. Forced Response Sensitivity of a Mistuned Rotor From an Embedded Compressor Stage

4. Besem FM, Kielb RE, Key NL. Forced Response Sensitivity of a Mistuned Rotor from an Embedded Compressor Stage. ASME. J. Turbomachinery. 2015;138(3):031002-031002-10. doi:10.1115/1.4031866.

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1. Effects of tip clearance on non-synchronous aerodynamic excitation of compressor rotor blades;Journal of Physics: Conference Series;2024-02-01

2. Structural Dynamics Applied to Rocket Engine Turbopumps;Synthesis Lectures on Mechanical Engineering;2022

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