Bomeman_Stephen_R.pdf (3.65 MB)

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

thesis

posted on 24.05.2021, 07:35 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

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Categories

Uncategorized content

Keywords

Airplanes -- Wings -- Vibration -- Measurement Airplanes -- Wings -- Mathematical models Airplanes -- Wings -- Design and construction Aerodynamics -- Technological innovations Vibration (Aeronautics)

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