Rotor Blade-to-Blade Wake Variability and Effect on Downstream Vane Response-Reference-Cited by-同舟云学术

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Rotor Blade-to-Blade Wake Variability and Effect on Downstream Vane Response

Published:2002-03 Issue:2 Volume:18 Page:456-464
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Sanders Albert J.¹,Fleeter Sanford¹

Affiliation:

1. Purdue University, West Lafayette, Indiana 47907

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/10.2514/2.5956

Reference9 articles.

1. Wake Dispersion in Turbomachines

2. Intra-Stator Transport of Rotor Wakes and Its Effect on Compressor Performance

3. Multistage Axial-Flow Turbomachine Wake Production, Transport, and Interaction

4. Three-dimensional unsteady flow in an axial flow turbine

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2. An experimental study of rotor-stator wake unsteadiness in a multistage axial compressor;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2020-12-08

3. Effects of Circumferential Nonuniformity in Compressor Flow Fields Including Vane Wake Variability;Journal of Propulsion and Power;2018-07

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