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Aviation History
1916
1916 - 1056.PDF
A GRAPHICAL METHOD OF DETERMINING BENDING MOMENTS IN CONTINUOUS BEAMS continued). (Strictly Copyright.) SI FJG6 Two £quAl Point LoAcis &( fi Fbint. • B.G.H.C.f* e/i'AgrAtir *f Bending Moment \an frrely supported sp*n,. K.VS mid' joint of C.H. . join fyK.aud K.C cutting perpendhut&M through T«u. in L& Nl. respectively N.L.M.Q. is the ciffing line Single Point La&din SMJ Position. B.G.C it diAgr-Ain of Bending flame/it on freely supported spAir. B'.C ItArAl/fltff B.C. K'.G. pAn\Uelta B!C. K2G. pArMto ac' pin K]c&^\it:u(tiJig perpmdiculws through T & u in i& M resfctfively. NLMQ is the closing line E Any Lo^dind" B.c.H c ts c/ididr&m of Bendind Moment . . :.:••• ' -. on1freely supportedefr&n TAe cenfre qfdr*vtty of&reA is c H c Li determined area, of B.G.H.C. * A fdll tfjniriiKiims must be in tht same units) r .\^\ , ^ A V A - BKI - fi'^Xg ri<2- oAX/7 . %*"•.!?"*, "Be" yew/ K'C 8.\?\icuttint pirpendictifara ttrroug/tT* u rVr L * M "NIMO» //ri dostttd line H 5 g H I I I 0\
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