An investigation of the conditions for the occurrence of flutter in aircraft and the development of criteria for the prediction and elimination of such flutter

An investigation of the conditions for the occurrence of flutter in aircraft and the development of criteria for the prediction and elimination of such flutter

A review is presented of the work done by other investigators on the effects of inertia couplings in producing flutter in control surfaces that are not mass balanced. The conclusion is reached that for the prevention of such flutter complete dynamic balance should always maintain. Flexural-torsio...

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Bibliographic Details
Main Author: Lombard, Albert Eaton
Format: Others
Published: 1939
Online Access:https://thesis.library.caltech.edu/2923/1/Lombard_ae_1939.pdf
Lombard, Albert Eaton (1939) An investigation of the conditions for the occurrence of flutter in aircraft and the development of criteria for the prediction and elimination of such flutter. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/80H8-TB52. https://resolver.caltech.edu/CaltechETD:etd-07182007-091133 <https://resolver.caltech.edu/CaltechETD:etd-07182007-091133>

Internet

https://thesis.library.caltech.edu/2923/1/Lombard_ae_1939.pdf
Lombard, Albert Eaton (1939) An investigation of the conditions for the occurrence of flutter in aircraft and the development of criteria for the prediction and elimination of such flutter. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/80H8-TB52. https://resolver.caltech.edu/CaltechETD:etd-07182007-091133 <https://resolver.caltech.edu/CaltechETD:etd-07182007-091133>

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