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: 62 of 171
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4 8 16 20
Angle of attack, a, deg
-se -nw -.M -.020 -.6 -92
Long/iud/no/-force ccoeff/cltf, C,
(b) Te = 0.4
Figure 13.- Continued.
e h i oe .16 .o sf8D4 0
P/tc/ing-momenf coefficient, C,
XILI'I't _ _ S - -
i ,,,deg _ - \ \
z -- 3/
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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/m1/62/: accessed May 21, 2019), University of North Texas Libraries, Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.