Design Optimization and Experimental Study of Tandem Impeller for Centrifugal Compressor

Author:

Ju Y. P.1,Zhang C. H.1

Affiliation:

1. Department of Fluid Machinery and Engineering, Xi’an Jiaotong University, 710049 Xi’an, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Reference26 articles.

1. Optimization of High Speed Centrifugal Compressor for a Micro Gas Turbine Based on CFD and FEM Analysis

2. WangH. L. “Optimization Design and Experimental Study of High Pressure Ratio Centrifugal Compressor,” Ph.D. Dissertation, Xi’an Jiaotong Univ., Xi’an, Shaanxi, PRC, July 2011.

3. BrentJ. A. “Single Stage Experimental Evaluation of Compressor Blading with Slots and Vortex Generators, Part III: Data and Performance for Stage 4,” NASA CR-72741, 1970.

4. Demonstration of Separation Delay with Glow Discharge Plasma Actuators

5. KochC. C.SmithL. H.Jr. “Experimental Evaluation of Outer Case Blowing or Bleeding of Single Stage Axial Flow Compressors, Part III: Performance of Blowing Insert Configuration No. 1,” NASA CR-54589, 1968.

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