2015-01-2080: Additional Considerations for Analytical Modeling of Rotor Blade Ice - Technical Paper

Event: SAE 2015 International Conference on Icing of Aircraft, Engines, and Structures

Authors

Roger J. Aubert

Bell Helicopter Textron

Abstract

Content: The entire process from ice accretion to ice impact with ice shedding in between still needs refinement. This paper presents key points illustrating the need for improvements in understanding the mechanical properties of ice accretion on helicopter rotor systems.

Meta Tags

Topics: Helicopters
Propellers and rotors
Icing and ice detection
Simulation and modeling

Affiliated or Co-Author: Bell Helicopter Textron

Details

DOI: https://doi.org/10.4271/2015-01-2080

Pages: 7

Citation: Aubert, R., "Additional Considerations for Analytical Modeling of Rotor Blade Ice," SAE Technical Paper 2015-01-2080, 2015, https://doi.org/10.4271/2015-01-2080.

Additional Details

Publisher: SAE International

Published: Jun 15, 2015

Product Code: 2015-01-2080

Content Type: Technical Paper

Language: English