Transient Response of a Multilayered Composite Rotating Airfoil Under Slicing-Impact Loading
Author:
Affiliation:
1. Nonlinear Dynamics, GE Aviation, Cincinnati, Ohio 45215
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052888
Reference41 articles.
1. Modeling Hail Ice Impacts and Predicting Impact Damage Initiation in Composite Structures
2. Modelling bird impacts on an aircraft wing – Part 1: Material modelling of the fibre metal laminate leading edge material with continuum damage mechanics
3. Modelling of Bird Strike on an Aircraft Wing Leading Edge Made from Fibre Metal Laminates – Part 2: Modelling of Impact with SPH Bird Model
4. Numerical prediction of damage in composite structures from soft body impacts
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