Generation of Vortex Lift Through Reduction of Rotor/Stator Gap in Turbomachinery-Reference-Cited by-同舟云学术

Generation of Vortex Lift Through Reduction of Rotor/Stator Gap in Turbomachinery

Published:2016-03 Issue:2 Volume:32 Page:472-485
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Du Lin¹,Sun Xiaofeng¹,Yang Vigor²

Affiliation:

1. Beijing University of Aeronautics and Astronautics, 100191 Beijing, People’s Republic of China

2. Georgia Institute of Technology, Atlanta, Georgia 30332

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.B35858

Reference53 articles.

1. DringR. P.BlairM. F.JoslynH. D.PowerG. D.VerdonJ. M. “The Effects of Inlet Turbulence and Rotor/Stator Interactions on the Aerodynamics and Heat Transfer of a Large-Scale Rotating Turbine Model: IV – Aerodynamic Data Tabulation,” NASA CR-4079, May 1986.

2. RaoK. V.DelaneyR. A. “Investigation of Unsteady Flow Through a Transonic Turbine Stage: Part I-Analysis,” AIAA Paper 1990-2408, 1990.

3. Investigation of Unsteady Flow Through a Transonic Turbine Stage: Data/Prediction Comparison for Time-Averaged and Phase-Resolved Pressure Data

4. Application of an unsteady Navier-Stokes solver to transonic turbinedesign

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