0 Given that 1800 lbf 300 lbflin. Roxo Rea o k loin L RBy = 6900 lbf Reg= 3900 lbf 15100 Ibe 11800 lbs 27 in -1800 - 3900 lbf 25,35o in lbf Y o in lbf 1-18.000 in-ibp a from the eauilibrium Conditions EMBO -> (Rcy) (30) +(1800) (10) = (300) (30) (15) -> Rcy = 3900 168 E Fyzo - RBY + Rey = (Boo) (30) + 1800. - RBy = 6900 lbf) Efn=0 - Since there is no hoarizontal load acting on the beam RBn= lonzo lbf
0 Given that 1800 lbf 300 lbflin. Roxo Rea o k loin L RBy = 6900 lbf Reg= 3900 lbf 15100 Ibe 11800 lbs 27 in -1800 - 3900 lbf 25,35o in lbf Y o in lbf 1-18.000 in-ibp a from the eauilibrium Conditions EMBO -> (Rcy) (30) +(1800) (10) = (300) (30) (15) -> Rcy = 3900 168 E Fyzo - RBY + Rey = (Boo) (30) + 1800. - RBy = 6900 lbf) Efn=0 - Since there is no hoarizontal load acting on the beam RBn= lonzo lbf
Section bw A2B ? Considen a section between AGB at a distance - n from SFx 11800 lbf Mr Sfx- - 1800 lbf Ma = - 1800 (2) at noin SFA = -1800 lbf : MA= 0 lof.in. at > = loin —> SFB = -1800 lbf ; MBP - 18,000 in-1bf Section blw Blo: Consider a section between B2C at a distance 1800 lbf x' from c. 1 SFX 300 lbflin. Sn = Gaoo - 1800 - 300 (n-10) k loin Mic= 6900 (2-10) - 1800 (2-0) - 300(n-10)2 to 6900 Ibe Me الب at na loin SFB = 5100 lbf ; MB = -18,000 in-lbe at na noin -> Sfo = -3900 lbf ; Mczo in lof & Shear fonce changing it's sign between B2 5гго 6960 - 1800 - 300 (n-10) zo n=27m - at x=27m from enda' Shear force is zego. when shear force is serio - Bending moment is min/man B Miman = 6900 (27-10) - 1800 (-o) ~150 (27-10) MOM >) Mimar = 25,350 in 1bf
- forom the Bending moment cacation INA INA Area m. I op lin Since the plane is y-anis; centawid of the y-axis plane aboot Neubral anis Symmetrical about the plane lies on 3 in Ay, Azyz from n-aois i A+Az k_ Bin C) = 3 inz zin A = y=% 1+3/2=215 in (Iccha bed= (193) = 2.25 in 4 3 in Az=(3) (s) a 3 in? Ilin " Y2 = 1/2 = 0.5 in . (I cal₂ = (3) (1)3 = 0.25 in" 5 = (3) (25) + (3) Cois) = 115 in from a anis. 3+3 5 = 1.5 in forom y-axis. :) INA: - Anea m'I of plane amina about Neutral anis INA = It Iz som of m'I's of the individual plane lamina's about N.A INA - [Ica,+ m (1-9)"). (fieca) t (4-5)
INA = (225 + (3)(2-5-15) 2 ) + (0-25 + 3) (05-15)) INA = 5.25 +3.25 INA = 8.5 iny Compressive Storess At maximum Bending moments; (At point o] o uppeor da - a bottom layer subjected. to tensile stress Mman = 25,350 in Ibe manimum tensile stress gging moment) tensile Stress [sman - Mmax) (Upa) = (25,350 (35) tensile INA (otensin) = (25,350) (15) = 4493.5 psi 8.5 o o comp) = 18060251350)(25) 8.5 745588 PS tensile AL point Bi | (18000)(215) [otensile] = 45 '5 = 5294.ll psi a - 5894all an (densia Compressin fotome 7 (18000) (15), 3176.47 Psi_ (come) from 0 0 2 - it is obsequed that [Stensiu]> [otensire tensiu] =5294. u psi) mon Cot B to come to <[o Comp Ja - man psi Tuss. 88 at D .