Analysis of the Ultimate Strength and Optimum Proportions of Multiweb Wing Structures Page: 25 of 35
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NACA TN 36355
TABLE II.- SPECIMEN DIMENSIONS - Concluded
(b) Fabricated beams.aSee figure 1(d).
Specimen h, tW, ts, bS, C, tT,
in. in. in. in. in. in.
(a)
101 .17 0.051 0.0835 1.63 5.73 0.083
102 3.15 .051 .083 2.04 6.94 .083
103 3.16 .051 .083 2.43 8.15 .083
104 3.17 .051 .082 35.22 10.58 .085
105 3.25 .051 .127 2.50 8.38 .17
106 3.25 .051 .127 3.12 10.24 .127
107 35.27 .051 .127 3.75 12.10 .127
108 3.26 .051 .126 4.98 15.84 .126
o109 3.38 .05 .187 3.75 12.15 .187
110 3.38 .051 .186 4.70 14.97 .186
111 3.38 .051 .186 5.64 17.79 .186
112 3.38 .051 .183 7.5~ 23.45 .183
113 3.62 .051 .512 6.25 19.66 .512
114 3.62 .051 .307 7.8*4 24.57 .307
115 3.61 .051 .509 9.40 g29.06 .309
116 3.61 .051 .10 12.54 38.46 .310
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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/m1/25/: accessed July 16, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.