Electric Analog Computer Study of Supersonic Flutter of Elastic Delta Wings

Electric Analog Computer Study of Supersonic Flutter of Elastic Delta Wings

This thesis presents a method for the solution of the supersonic flutter problem for elastic delta wings with supersonic leading edges. In Part I, the necessary aerodynamic equations are developed, first in integral form, and then in a power series expansion in order to obtain a practical express...

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Bibliographic Details
Main Author: Basin, Michael Abram
Format: Others
Published: 1954
Online Access:https://thesis.library.caltech.edu/4659/1/Basin_ma_1954.pdf
Basin, Michael Abram (1954) Electric Analog Computer Study of Supersonic Flutter of Elastic Delta Wings. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/FHFK-QR87. https://resolver.caltech.edu/CaltechETD:etd-11252003-111202 <https://resolver.caltech.edu/CaltechETD:etd-11252003-111202>

Internet

https://thesis.library.caltech.edu/4659/1/Basin_ma_1954.pdf
Basin, Michael Abram (1954) Electric Analog Computer Study of Supersonic Flutter of Elastic Delta Wings. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/FHFK-QR87. https://resolver.caltech.edu/CaltechETD:etd-11252003-111202 <https://resolver.caltech.edu/CaltechETD:etd-11252003-111202>

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