Structural Dynamics and Aeroelasticity
The course focuses on applying quantum mechanics and mechanical vibrations to aerospace engineering problems. It covers deriving differential equations of motion using Lagrange’s equation and Hamilton’s principle, as well as analyzing aircraft wing divergence, flutter, and response. The course also discusses the impact of gust loads on aircraft design and explores the use of novel methods and technologies, including non-linear control systems. Engineers and scientists involved in aeronautical structures design, operation, and assessment are encouraged to attend for a balance of theory and practice.