Analysis of the Ultimate Strength and Optimum Proportions of Multiweb Wing Structures Page: 27 of 35
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NACA TN 3633
TABLE III.- RATIOS OF SPECIMEN DIMENSIONS - Concluded
(b) Fabricated beams.
Specimen h/tS bS/tS tW/tS bwt /t
(a)
101 38.2 19.6 0.6 59 3.0
102 38.0 24.6 .6 59 2.4
103 38.1 29.3 .6 59 2.0
104 38.6 39.3 .6 59 1.5
105 25.6 19.7 .4 59 3.0
106 25.6 24.6 .4 59 2.4
107 25.8 29.5 .4 59 2.0
108 25.9 39.6 .4 59 1.5
o109 18.1 20.0 .3 59 3.0
110 18.1 25.2 .3 59 2,3
11l 18.2 30.3 .3 59 2.0
112 18.5 41. .3 59 1.4
113 11.3 20.0 .2 59 3.0
u4 11.8 25.5 .2 59 2.3
115 11.7 30.4 .2 59 2.0
116 11.7 40.5 .2 59 1.5
aSee figure 1(d).26
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Rosen, B. Walter. Analysis of the Ultimate Strength and Optimum Proportions of Multiweb Wing Structures, report, March 1956; (https://digital.library.unt.edu/ark:/67531/metadc57902/m1/27/?rotate=270: accessed July 17, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.