Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 161
70 Bearing stress on bolt _ .25 (.0930+ .049)109. Wing Fitting—Fig. 93 is a wing-spar fitting developed by theAirplane Design Section. This is essentially a box fitting and illustratesvery clearly how eccentricities of struts and wires may be avoided. Itwill be noted that the lines of action of the… … Fig. 93. Wing Spar Fittings Without Eccentricities 142 CHAPTER V AIRPLANE CHASSIS 110. General Considerations—Until recently comparatively littlehad been done on the accurate stress analysis of chassis. Consequently,there has been less opportunity to corroborate by static test the resultsof the…
Airplanes
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