Linearized transonic flow about nonlifting, thin symmetric airfoils

Linearized transonic flow about nonlifting, thin symmetric airfoils

Transonic flow about symmetric, non-lifting airfoils is treated by solving an approximate linear differential equation of mixed type in place of the exact small-perturbation equations. The pressure distribution and drag coefficient are obtained in closed form for power series airfoils. The technique...

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Bibliographic Details
Main Author: Petty, James Sibley
Format: Others
Published: 1963
Online Access:https://thesis.library.caltech.edu/4835/1/Petty_js_1963.pdf
Petty, James Sibley (1963) Linearized transonic flow about nonlifting, thin symmetric airfoils. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/3ZC0-7Y26. https://resolver.caltech.edu/CaltechETD:etd-12072005-135856 <https://resolver.caltech.edu/CaltechETD:etd-12072005-135856>

Internet

https://thesis.library.caltech.edu/4835/1/Petty_js_1963.pdf
Petty, James Sibley (1963) Linearized transonic flow about nonlifting, thin symmetric airfoils. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/3ZC0-7Y26. https://resolver.caltech.edu/CaltechETD:etd-12072005-135856 <https://resolver.caltech.edu/CaltechETD:etd-12072005-135856>

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