Results of experiments made to determine (1) effect of changing upper and lower camber of thick aerofoils of uniform section, (2) effect of thickening center and thinning tips of thin aerofoil, (3) effect of adding convex lower surface to tapered section, (4) effect of changing mean thickness with constant center and tip sections, and (5) effect of varying chord along span.
The aerodynamic properties of thick aerofoils suitable for internal bracing
Nat. Advisory Committee Aeronautics, report
1920
26 pages
29 Figs.
Report
English
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The aerodynamic properties of thick aerofoils suitable for internal bracing
Engineering Index Backfile | 1920
|The aerodynamic properties of thick aerofoils
Engineering Index Backfile | 1922
|Aerodynamic characteristics of aerofoils
SLUB | 1928