Modeling and Dynamic Analysis of Shrouded Turbine Blades in Aero-Engines-Reference-Cited by-同舟云学术

Modeling and Dynamic Analysis of Shrouded Turbine Blades in Aero-Engines

Published:2016-01 Issue:1 Volume:29 Page:04015021
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Nan Guofang¹

Affiliation:

1. Lecturer, Univ. of Shanghai for Science and Technology, 516 Jun Gong Rd., Shanghai 200093, P.R. China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000510

Reference23 articles.

1. A model for the characterization of friction contacts in turbine blades;Allara M.;J. Sound Vib.,2009

2. Stability Analysis of Rotating Blade Vibration due to Torsional Excitation

3. Chan Y. J. (2009). “Variability of blade vibration in mistuned bladed discs.” Ph.D. thesis Department of Mechanical Engineering Imperial College London.

4. Periodic Response of Blades Having Three-Dimensional Nonlinear Shroud Constraints

5. VIBRATION ANALYSIS OF ELASTICALLY SUPPORTED TURBOMACHINERY BLADES BY THE MODIFIED DIFFERENTIAL QUADRATURE METHOD

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