Aerodynamic characteristics of 24 airfoils are given for speeds of 0. 5, 0.65, 0.8, 0.95 and 1.08 times speed of sound as measured in openjet air stream using models of 1-in. chord; nine members of Standard R.A.F. airfoil used by Army and Navy for propeller design, and five members of Clark Y family differing only in thickness tested; R.A.F. family in which position of maximum ordinate is varied; combined groups; group consisting of three geometrical forms, flat plate, wedge, and segment of right circular cylinder.
Aerodynamic characteristics of twenty-four airfoils at high speeds
Nat. Advisory Committee Aeronautics -- Report
1929
32 pages
45 Figs.
Report
English
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Aerodynamic characteristics of airfoils at high speeds
Engineering Index Backfile | 1925
|Aerodynamic characteristics of airfoils at high speeds
TIBKAT | 1928
|Aerodynamic Characteristics of Airfoils at High Speeds
NTRS | 1925
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