Experimental Investigation of Rotor-Inlet Guide Vane Interactions in Transonic Axial-Flow Compressor-Reference-Cited by-同舟云学术

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Experimental Investigation of Rotor-Inlet Guide Vane Interactions in Transonic Axial-Flow Compressor

Published:2000-05 Issue:3 Volume:16 Page:421-430
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/10.2514/2.5606

Reference4 articles.

1. IGV–Rotor Interaction Analysis in a Transonic Compressor Using the Navier–Stokes Equations

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2. Numerical investigation of plasma actuator induced forcing direction on the performance of a low-speed isolated axial compressor rotor;Journal of Electrostatics;2022-07

3. The Effect of Variable Inlet Guide Vanes on the Performance of Military Engine Fan;Lecture Notes in Mechanical Engineering;2021

4. Emulation of Frequency and Mode Shape Variation of As-manufactured Airfoils with Eigenvalue Veering and Crossing;AIAA Scitech 2019 Forum;2019-01-06

5. Criteria for designing low-loss and wide operation range variable inlet guide vanes;Aerospace Science and Technology;2018-09

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