Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 115
neness ratio between 2.0 and 5.0.diameter was located at 40 per cent of the long axisSince the maximum diameter of the strut section of this airplane is at38 per cent of the long axis from the nose it will be accurate enough touse these formulas. The actual length of the front struts is 53^ in. and… … 96 Art. 76 Stress Table TABLE X DIMENSIONS OF STRUTS Struts Front and RearOuter AverageLength 54 in. Short Dia- Long Dia-meter d meter ab IV. in. 4V, in. FinenessRatio b/d 3.78 Front and RearIntermediate. . 54 in. l15/32 in. 49/1(J in. 3.12 PROPERTIES OF STRUT SECTIONS Struts I Long Axis p Long…
Airplanes
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