Reduction of Aerodynamic Forcing Through Introduction of Stator Asymmetry in Axial Compressors-Reference-Cited by-同舟云学术

Reduction of Aerodynamic Forcing Through Introduction of Stator Asymmetry in Axial Compressors

Published:2016-01 Issue:1 Volume:32 Page:134-141
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Monk David J.¹,Key Nicole L.¹,Fulayter Roy D.²

Affiliation:

1. School of Mechanical Engineering, Purdue University, West Lafayette, Indiana 47907

2. Rolls–Royce Corporation, Indianapolis, Indiana 46225

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.B35704

Reference16 articles.

1. PanningL.SextroW.PoppK. “Optimization of the Contrast Geometry Between Turbine Blades and Underplatform Dampers with Respect to Friction Damping,” American Soc. of Mechanical Engineers GT2002-30429, Fairfield, NJ, 2002.

2. Forced Response Analysis of an Aerodynamically Detuned Supersonic Turbomachine Rotor

3. KempR. H.HirschbergM. H. “Theoretical and Experimental Analysis of the Reduction of Rotor Blade Vibration in Turbomachinery Through the Use of Modified Stator Vane Spacing,” NACA Rept. TN-4373, 1958.

4. Investigation on the Effect of Asymmetric Vane Spacing on the Reduction of Rotor Blade Vibration

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