Analysis Method for Inertial Particle Separator
Author:
Affiliation:
1. King Fahd University of Petroleum and Minerals, Dhahran 31261, Saudi Arabia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.20245
Reference34 articles.
1. Life prediction of helicopter engines fitted with dust filters
2. Development of an advanced vaneless inlet particle separator for helicopter engines
3. Analysis of a split-flow inertial particle separator by finite elements
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