Flutter Generation and Control Using Mistuning in a Turbine Rotating Rig-Reference-Cited by-同舟云学术

Flutter Generation and Control Using Mistuning in a Turbine Rotating Rig

Published:2019-02 Issue:2 Volume:57 Page:782-795
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Corral Roque¹,Beloki Josu²,Calza Paolo³,Elliott Robert⁴

Affiliation:

1. Industry of Turbopropellers S.A.U., Advanced Engineering Direction, 28168 Madrid, Spain

2. Center of Aeronautical Technologies, Fluid Dynamics Center, 48170 Zamudio, Spain

3. Avio Aero, Engineering Technologies, 10040 Torino, Italy

4. Coquetdale Engineering Consultancy Ltd., Morpeth, England NE65 7EZ, United Kingdom

Funder

FP7 Transport

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056943

Reference42 articles.

1. Experimental Investigation of Mode Shape Sensitivity of an Oscillating Low-Pressure Turbine Cascade at Design and Off-Design Conditions

2. A Test Facility for the Investigation of Steady and Unsteady Transonic Flows in Annular Cascades

3. FranssonT. H.VerdonJ. M. “Updated Report on Standard Configurations for Unsteady Flow,” Tech. Rept. Royal Inst. of Technology, Stockholm, Sweden, 1992, http://www.egi.kth.se/ekv/stck.

4. Rotating Stall Observations in a High Speed Compressor: Part 1 — Experimental Study

5. Experimental and Computational Fluid Dynamics Based Determination of Flutter Limits in Supersonic Space Turbines

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