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- W1539951806 abstract "has been customary to calculate the strength of the rear wing beam for the 'high speed' condition on the assumption that the center of pressure was at 0.50 of the wing chord. It can be shown that this assumption is not justified, regardless of the utility of a 'high speed' condition in strength calculations (p. 1)." @default.
- W1539951806 created "2016-06-24" @default.
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- W1539951806 date "1922-04-01" @default.
- W1539951806 modified "2023-09-25" @default.
- W1539951806 title "Center of pressure coefficients for airfoils at high speeds" @default.
- W1539951806 hasPublicationYear "1922" @default.
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