Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90 degrees Page: 20 of 44
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REPORT- 1263-NATIONAL ADVISORY COMMITTEE FOR- AERONAUTICS
16-
40C
.30I
t-
6--
u .20
c
C,
IL
wAngle of attack, a, deg
(a) T"= 0.91; /.7R-- 80
FIGURE 10.-Comparison of advance ratios for various configurations at constant thrust through angle-of-attack range.
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Kuhn, Richard E. & Draper, John W. Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90 degrees, report, 1956; (https://digital.library.unt.edu/ark:/67531/metadc60654/m1/20/: accessed April 24, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.