A study of flutter in one degree of freedom

A study of flutter in one degree of freedom

The authors have attempted to develop a theoretical means of determining the amount of aerodynamic damping, positive or negative, existing on a symmetrical airfoil having freedom to oscillate only about an axis parallel to the span and on the zero camber line. Variables considered were oscillating f...

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Bibliographic Details
Main Authors: Kiergan, Nova Babb, Tomamichel, Jack Jones
Format: Others
Published: 1942
Online Access:https://thesis.library.caltech.edu/4653/1/Kiergan_nb_1942.pdf
Kiergan, Nova Babb and Tomamichel, Jack Jones (1942) A study of flutter in one degree of freedom. Engineer's thesis, California Institute of Technology. doi:10.7907/NX9K-JT57. https://resolver.caltech.edu/CaltechETD:etd-11242008-082928 <https://resolver.caltech.edu/CaltechETD:etd-11242008-082928>

Internet

https://thesis.library.caltech.edu/4653/1/Kiergan_nb_1942.pdf
Kiergan, Nova Babb and Tomamichel, Jack Jones (1942) A study of flutter in one degree of freedom. Engineer's thesis, California Institute of Technology. doi:10.7907/NX9K-JT57. https://resolver.caltech.edu/CaltechETD:etd-11242008-082928 <https://resolver.caltech.edu/CaltechETD:etd-11242008-082928>

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