Cited by 37Bladed Disk Vibration DynamicsMechanical Behavior of CompositesTurbomachinery Performance and Optimization

The DOI matches its Crossref record.

Analytical and Experimental Simulation of Fan Blade Behavior and Damage Under Bird Impact

Teichman, H. C., Tadros, R. N.·1991·Journal of Engineering for Gas Turbines and Power

Abstract

An extensive analytical and experimental program has been undertaken to investigate the Foreign Object Damage resistance capabilities of external components for small gas turbofan engines. A transient nonlinear impact analysis has been used to predict the structural response of fan blades under bird ingestion conditions. This analysis is based on finite elements, a three-dimensional bird load model, and an interactive structure-to-bird contact algorithm. Experiments were designed and carried out to record large blade deformations during bird impact, and were used to validate and calibrate the analytical models. The analytical models and testing program are described, and dominant fan blade response and failure modes are presented. Predicted results demonstrate good correlation with tests. Analysis application to fan blade design and other engine components is recommended.

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Crossref · 10.1115/1.2906281

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Metadata

Authors
Teichman, H. C., & Tadros, R. N.
Affiliations
Pratt and Whitney Canada (Canada) (CA)
Venue
Journal of Engineering for Gas Turbines and Power
Published
1991-10-01
Volume
113
Issue
4
Pages
582-594
ISSN
  • 0742-4795 (ISSN-L)
  • 1528-8919
OpenAlex
W1977297682
Cited by
37
References
0
Citations by year
2025: 1 · 2024: 2 · 2023: 3 · 2022: 1 · 2021: 2 · 2019: 1 · 2018: 1 · 2015: 5 · 2014: 1 · 2013: 4 · 2012: 1
FWCI
0.00
Type
journal article
Language
en
Open access
closed
Locations
Journal of Engineering for Gas Turbines and Power (publishedVersion)
Funders
U.S. Department of Defense
Topics
  • Physical Sciences › Engineering › Mechanical Engineering › Bladed Disk Vibration Dynamics
  • Physical Sciences › Engineering › Mechanics of Materials › Mechanical Behavior of Composites
  • Physical Sciences › Engineering › Aerospace Engineering › Turbomachinery Performance and Optimization
Keywords
foreign object damage, fan blades, bird ingestion, blade deformation, failure modes, structural response prediction, model validation

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