Variable Stator Vane Penny Gap Aerodynamic Measurements and Numerical Analysis in an Annular Cascade Wind Tunnel

Author:

Pohl Daniel1,Janssen Johannes1,Jeschke Peter1,Halcoussis Alexander2,Wolf Hannes2

Affiliation:

1. Institute of Jet Propulsion and Turbomachinery, RWTH Aachen University

2. MTU Aero Engines AG

Publisher

Gas Turbine Society of Japan

Subject

Mechanical Engineering

Reference21 articles.

1. Cumpsty, N. A. and Greitzer, E. M., 2004, “Ideas and Methods of Turbomachinery Aerodynamics: A Historical View,” Journal of Propulsion and Power, Vol. 20, No. 1, pp. 15-26.

2. Wellborn, Steven R. and Okiishi, Theodore H., 1996, “Effects of Shrouded Stator Cavity Flows on Multistage Axial Compressor Aerodynamic Performance,” NASA-CR-198536, E-10465, NAS 1.26:198536.

3. Mattingly, J. D., Heiser, W. H. and Pratt, D. T., 2002, “Aircraft Engine Design,” American Institute of Aeronautics and Astronautics.

4. Ludwig, Lawrence P. and Bill, Robert C., 1980, “Gas path sealing in turbine engines,” Asle Transactions, 23:1, pp. 1-22.

5. Hawkins, R. M., 1966, “Development of compressor end seals, stator interstage seals, and stator pivot seals in advanced air breathing propulsion systems,” Semiannual report, 1 Jan.-30 Jun. 1966.

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