The effects of nonstationary aerodynamics of the rigid-body dynamic stability of an airplane

The effects of nonstationary aerodynamics of the rigid-body dynamic stability of an airplane

A first order in frequency theory is developed for the aerodynamic loads on a harmonically oscillating thin wing of finite aspect ratio in a subsonic compressible flow. The downwash in the vicinity of a horizontal tail behind such a wing is also evaluated to the same order in frequency. The results...

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Bibliographic Details
Main Author: Statler, Irving C.
Format: Others
Published: 1956
Online Access:https://thesis.library.caltech.edu/2783/1/Statler_ic_1956.pdf
Statler, Irving C. (1956) The effects of nonstationary aerodynamics of the rigid-body dynamic stability of an airplane. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/1EHQ-B547. https://resolver.caltech.edu/CaltechETD:etd-06302004-095128 <https://resolver.caltech.edu/CaltechETD:etd-06302004-095128>

Internet

https://thesis.library.caltech.edu/2783/1/Statler_ic_1956.pdf
Statler, Irving C. (1956) The effects of nonstationary aerodynamics of the rigid-body dynamic stability of an airplane. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/1EHQ-B547. https://resolver.caltech.edu/CaltechETD:etd-06302004-095128 <https://resolver.caltech.edu/CaltechETD:etd-06302004-095128>

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