Radial Migration of Shed Vortices in a Transonic Rotor Following a Wake Generator: A Comparison Between Time Accurate and Average Passage Approaches

Author:

Turner Mark G.1,Gorrell Steven E.2,Car David3

Affiliation:

1. University of Cincinnati

2. Brigham Young University

3. Air Force Research Laboratory, Wright-Patterson Air Force Base

Abstract

This paper shows a comparison of an unsteady simulation using turbo and an average passage simulation for a two blade row configuration consisting of a wake generator followed by a transonic rotor. Two spacings were simulated, both close and far. The unsteady results compare well with experiment especially for the profile of efficiency difference between close and far. An analysis of results helps to explain the unusual profile seen experimentally that is due to the radial migration of wake generator shed vortices with negative radial velocities near the tip. In addition, different components of the average passage body forces (deterministic stresses) are explored that shows the main terms are the axial momentum and the metal blockage.

Publisher

ASME International

Subject

Mechanical Engineering

Reference19 articles.

1. The Effects of Blade-Row Spacing on the Flow Capacity of a Transonic Rotor;Chriss

2. Analysis of a Highly Loaded, Transonic, Inlet Compressor Stage: Isolated and Multi-Stage Performance;Car

3. Gorrell, S. E. , 2001, “An Experimental and Numerical Investigation of Stator-Rotor Interactions in a Transonic Compressor,” Ph.D. thesis, Mechanical Engineering, Iowa State University, Ames, IA.

4. Stator-Rotor Interactions in a Transonic Compressor—Part 2: Description of a Loss-Producing Mechanism;Gorrell;ASME J. Turbomach.

5. Law, C. H., and Wennerstrom, A. J., 1989, “Two Axial Compressor Designs for a Stage Matching Investigations,” Paper No. AF-WAL-TR-89-2005.

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