The lift of thin airfoils at high-subsonic speeds

The lift of thin airfoils at high-subsonic speeds

Experimental results are presented for the lift characteristics of thin, two-dimensional airfoils at high-subsonic speeds and small angles of attack. Symmetrical airfoils with different locations of maximum thickness were investigated using a surface pressure probe technique which should find use in...

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Bibliographic Details
Main Author: Willmarth, William W.
Format: Others
Published: 1954
Online Access:https://thesis.library.caltech.edu/272/1/Willmarth_ww_1954.pdf
Willmarth, William W. (1954) The lift of thin airfoils at high-subsonic speeds. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/DFFC-8041. https://resolver.caltech.edu/CaltechETD:etd-01222004-114509 <https://resolver.caltech.edu/CaltechETD:etd-01222004-114509>

Internet

https://thesis.library.caltech.edu/272/1/Willmarth_ww_1954.pdf
Willmarth, William W. (1954) The lift of thin airfoils at high-subsonic speeds. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/DFFC-8041. https://resolver.caltech.edu/CaltechETD:etd-01222004-114509 <https://resolver.caltech.edu/CaltechETD:etd-01222004-114509>

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