Spinning symmetric missiles in a nonlinear aerodynamic field

Spinning symmetric missiles in a nonlinear aerodynamic field

The case of a spinning symmetric body flying at a constant speed where the aerodynamic restoring moment is an arbitrary function of the angle of attack is examined. The analysis is twofold: first, the general problem is discussed, in suitable nondimensional form, to establish the generalized stabili...

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Bibliographic Details
Main Author: Mantle, Peter J.
Format: Others
Published: 1964
Online Access:https://thesis.library.caltech.edu/3847/1/Mantle_pj_1969.pdf
Mantle, Peter J. (1964) Spinning symmetric missiles in a nonlinear aerodynamic field. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/YXWV-VV41. https://resolver.caltech.edu/CaltechETD:etd-10012002-102742 <https://resolver.caltech.edu/CaltechETD:etd-10012002-102742>

Internet

https://thesis.library.caltech.edu/3847/1/Mantle_pj_1969.pdf
Mantle, Peter J. (1964) Spinning symmetric missiles in a nonlinear aerodynamic field. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/YXWV-VV41. https://resolver.caltech.edu/CaltechETD:etd-10012002-102742 <https://resolver.caltech.edu/CaltechETD:etd-10012002-102742>

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