NASA NTRS · 20030064921
Aeroelastic Problems of Airplane Design
Abstract
The technical memorandum briefly summarizes the growth of interest in aeroelastic phenomena as aircraft speed increased and wing designs changed for faster aircraft. Different types of aircraft vibrations are then introduced, and the mathematical basis for the theory behind them is described. Special attention is given to static oscillations, wing flutter, and the flutter of skin panels. The last section of the memorandum deals with the prevention of flutter by design specifications.
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Kuessner, H. G.. 1956-11-01. Aeroelastic Problems of Airplane Design. https://ntrs.nasa.gov/citations/20030064921
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