Analysis of a split-flow inertial particle separator by finite elements
Author:
Affiliation:
1. Pratt & Whitney Canada, Ontario, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45097
Reference10 articles.
1. A transonic quasi-3D analysis for gas turbine engines including split-flow capability for turbofans
2. Particle drag and heat transfer in rocket nozzles
3. Measured Particle Rebound Characteristics Useful for Erosion Prediction
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