Unit-step motion of a wide delta-wing

Unit-step motion of a wide delta-wing

The effect on a wide delta wing in supersonic flight of the sudden imposition of a small velocity perturbation normal to the plane of the wing is considered. The resulting pressure field on the wing is found in closed form in terms of elementary functions. The corresponding solution for the infinite...

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Bibliographic Details
Main Author: Parkinson, Geoffrey Vernon
Format: Others
Published: 1951
Online Access:https://thesis.library.caltech.edu/1628/1/Parkinson_gv_1951.pdf
Parkinson, Geoffrey Vernon (1951) Unit-step motion of a wide delta-wing. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/73TW-ZE47. https://resolver.caltech.edu/CaltechETD:etd-05052006-090936 <https://resolver.caltech.edu/CaltechETD:etd-05052006-090936>

Internet

https://thesis.library.caltech.edu/1628/1/Parkinson_gv_1951.pdf
Parkinson, Geoffrey Vernon (1951) Unit-step motion of a wide delta-wing. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/73TW-ZE47. https://resolver.caltech.edu/CaltechETD:etd-05052006-090936 <https://resolver.caltech.edu/CaltechETD:etd-05052006-090936>

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