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A New Dynamic Finite Element Formulation with Applications to Composite Aircraft Wings

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posted on 24.05.2021, 07:35 authored by Stephen R. Bomeman
A New Dynamic Finite Element Formulation with Applications to Composite Aircraft Wings

History

Language

eng

Degree

Master of Applied Science

Program

Mechanical and Industrial Engineering

Granting Institution

Ryerson University

LAC Thesis Type

Thesis

Thesis Advisor

Seyed M. Hashemi

Usage metrics

Mechanical and Industrial Engineering (Theses)Mechanical and Industrial Engineering (Theses)

Categories

Keywords

Airplanes -- Wings -- Vibration -- MeasurementAirplanes -- Wings -- Mathematical modelsAirplanes -- Wings -- Design and constructionAerodynamics -- Technological innovationsVibration (Aeronautics)

Licence

In Copyright

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