Effects of planform curvature in supersonic wings

Effects of planform curvature in supersonic wings

In this thesis a method is developed for calculating supersonic wings with curved subsonic leading edges. The linearized theory is used throughout the thesis. The wing with the curved subsonic leading edges is transformed into a wing with straight subsonic leading edges by means of a transformati...

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Bibliographic Details
Main Author: Hoeijmakers, Hendrik Willem Marie
Format: Others
Published: 1974
Online Access:https://thesis.library.caltech.edu/4314/1/Hoeijmakers_hwm_1974.pdf
Hoeijmakers, Hendrik Willem Marie (1974) Effects of planform curvature in supersonic wings. Engineer's thesis, California Institute of Technology. doi:10.7907/6DFV-0J65. https://resolver.caltech.edu/CaltechETD:etd-10302003-092227 <https://resolver.caltech.edu/CaltechETD:etd-10302003-092227>

Internet

https://thesis.library.caltech.edu/4314/1/Hoeijmakers_hwm_1974.pdf
Hoeijmakers, Hendrik Willem Marie (1974) Effects of planform curvature in supersonic wings. Engineer's thesis, California Institute of Technology. doi:10.7907/6DFV-0J65. https://resolver.caltech.edu/CaltechETD:etd-10302003-092227 <https://resolver.caltech.edu/CaltechETD:etd-10302003-092227>

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