Comparison of theoretical and experimental response of a single-mode elastic system in hydrodynamic impact /

Comparison of theoretical and experimental response of a single-mode elastic system in hydrodynamic impact / Robert W. Miller and Kenneth F. Merten.

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Hydrodynamic impact tests wre made on an elastic model approximating a two-mass - spring system which had a ratio of sprung mass to hull mass of 0.6 and a natural frequency of 3.0 cycles per second. Tests were made at two combinations of trim and flight-path angles for a range of flight-path velocit...

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Main Author: Miller, Robert W.
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Merten, Kenneth F.
Other title:Technical report archive and image library.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1951.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 2343.
Subjects:
Seaplanes > Hydrodynamics.
Seaplanes > Landing.
Elasticity.
Impact > Testing.

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Call Number: Y 3.N 21/5:6/2343
Y 3.N 21/5:6/2343 Available Place a Hold

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