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Aeroelastic Problems of Airplane DesignThe 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.
Document ID
20030064921
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Kuessner, H. G. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
September 7, 2013
Publication Date
November 1, 1956
Publication Information
Publication: Zeitschrift fuer Flugwissenschaften 3 Jahrgang, Heft 1
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-TM-1402
Report Number: NACA-TM-1402
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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