Full-Scale Testing of a Centrifugally Powered Pneumatic De-Icing System for Helicopter Rotor Blades
Author:
Affiliation:
1. Pennsylvania State University, University Park, Pennsylvania 16802
2. Invercon, LLC, State College, Pennsylvania 16801
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033965
Reference8 articles.
1. Aircraft icing
2. Helicopter Rotor Icing Protection Methods
3. Advanced pneumatic impulse ice protection system (PIIP) for aircraft
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