W. G. Molyneux
Abstract
Consideration is given to areas in which wind tunnel tests on scale representative aeroelastic models provide useful information on the behaviour of an aircraft. The basic features of techniques adopted for response measurements on aeroelastic models are described and their applications and limitations discussed.
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Consideration is given to areas in which wind tunnel tests on scale representative aeroelastic models provide useful information on the behaviour of an aircraft. The basic features of techniques adopted for response measurements on aeroelastic models are described and their applications and limitations discussed.
Key concepts: Aeroelasticity, Wind tunnel, Scale model, Engineering, Structural engineering, Scale (ratio), Computer science, Marine engineering