Analysis of Wind-Tunnel Tests to a Mach Number of 0.90 of a Four-Engine Propeller-Driven Airplane Configuration Having a Wing With 40 Degrees of Sweepback and an Aspect Ratio of 10 Page: 74 of 171
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.12 :O8 .04
A Cm wing
(b) Inboard flapm deflected.
Figure 20.- Concluded.
160 .4 1ix. 01 .L 40 O O -'-1-1-
Both propellers Inboard propeller only Outoard propeller only
I I I t . I I II I 1 [1 I I
. ..-.-.-- -I-- - - I - - -l -
0 -04 --08
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Edwards, George G.; Buell, Donald A.; Demele, Fred A. & Sutton, Fred B. Analysis of Wind-Tunnel Tests to a Mach Number of 0.90 of a Four-Engine Propeller-Driven Airplane Configuration Having a Wing With 40 Degrees of Sweepback and an Aspect Ratio of 10, report, September 1956; (https://digital.library.unt.edu/ark:/67531/metadc56014/m1/74/: accessed May 23, 2019), University of North Texas Libraries, Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.