# Example 10.1 IPS(deg) tpi = 5.0 /in p = 1/ tpi ; in L1 = 2 * p ; in dth = p/2 ; in d = 1.0 in dm = d - p/2 ; in len = atan(L1 / pi() / dm) ; deg f = 0.12 fstart = (4/3) * f fc = f a = 14.5 deg an = atan(tan(a) * cos(len)) ; deg W1 = 1000.0 lbf # dc = d - p/2 dc = 1.5 in T_up1 = (W1 * dm / 2) * (fstart * pi() * dm + L1 * cos(an)) / \ (pi() * dm * cos(an) - fstart * L1) + W1 * fc * dc / 2 ; lbf in T_down1 = (W1 * dm / 2) * (fstart * pi() * dm - L1 * cos(an)) / \ (pi() * dm * cos(an) + fstart * L1) + W1 * fc * dc / 2 ; lbf in # DYNAMIC tpi = 5.0 /in p = 1/ tpi ; in L1 = 2 * p ; in dth = p/2 ; in d = 1.0 in dm = d - p/2 ; in len = atan(L1 / pi() / dm) ; deg f = 0.09 fstart = (4/3) * f fc = f a = 14.5 deg an = atan(tan(a) * cos(len)); deg W1 = 1000.0 lbf # dc = d - p/2 dc = 1.5 in T_up2 = (W1 * dm / 2) * (fstart * pi() * dm + L1 * cos(an)) / \ (pi() * dm * cos(an) - fstart * L1) + W1 * fc * dc / 2 ; lbf in T_down2 = (W1 * dm / 2) * (fstart * pi() * dm - L1 * cos(an)) / \ (pi() * dm * cos(an) + fstart * L1) + W1 * fc * dc / 2 ; lbf in # NO FRICTION tpi = 5.0 /in p = 1/ tpi ; in L1 = 2 * p ; in dth = p/2 ; in d = 1.0 in dm = d - p/2 ; in len = atan(L1 / pi() / dm) ; deg f = 0.0 fstart = (4/3) * f fc = f a = 14.5 deg an = atan(tan(a) * cos(len)); deg W1 = 1000.0 lbf # dc = d - p/2 dc = 1.5 in T_up3 = (W1 * dm / 2) * (fstart * pi() * dm + L1 * cos(an)) / \ (pi() * dm * cos(an) - fstart * L1) + W1 * fc * dc / 2 ; lbf in T_down2 = (W1 * dm / 2) * (fstart * pi() * dm - L1 * cos(an)) / \ (pi() * dm * cos(an) + fstart * L1) + W1 * fc * dc / 2 ; lbf in err = T_up3 / T_up2 # Example 10.2 Sp = 380.0 Mpa F1 = 4.5 kN FOS = 4.0 Fdesign = F1 * FOS ; kN A1 = Fdesign / Sp ; mm^2 dM10X15 = 10.0 mm AM10X15 = 58.0 mm^2 Fi = 0.9 * AM10X15 * Sp ; kN T1 = 0.2 * Fi * dM10X15 ; N m # Example 10.3 Sp = 85.0 ksi Sy = 92.0 ksi d = 0.5000 in A1 = 0.1419 in^2 Fi_rough = A1 * Sp ; lbf FOSFi = 1.59 Fi = A1 * Sp / FOSFi ; lbf m1 = 0.4000 Ff = m1 * Fi ; lbf F1 = 2 * Ff ; lbf Fshear = 2 * (0.58 * Sy) * pi() * d^2 / 4 ; lbf # Example 10.4 BEGIN FOS = 6.0 F1 = 24.0 kN Fdesign = FOS * F1 ; kN FD = 87.3 kN FE = FD / 4 ; kN xF = 500.0 mm xE = 100.0 mm xD = 400.0 mm SumM = xF * Fdesign - xE * FE - 2 * xD * FD ; kN mm Sp = 650.0 Mpa At = FD / Sp ; mm^2 END Solve(SumM, FD) # Example 10.5 BEGIN A1 = 100 mm^2 F1 = 87.3 kN V1 = 81.5 kN s1 = F1 / A1 ; Mpa t = V1 / A1 ; Mpa se = (s1^2 + 3 * t^2)^(1/2) ; Mpa Sp = 650.0 Mpa error = se - Sp ; Mpa d = (4 * A1 / pi())^(1/2) ; mm END solve(error, A1) # Example 10.6 IPS(deg) BEGIN # (a) Fmax = 3000 lbf Kf = 3.8 At = 0.1419 in^2 sa = Fmax * Kf / 2 / At ; ksi sm = sa Sp = 37.0 ksi error1 = sa - Sp ; ksi # (b) Sp = 85.0 ksi At = 0.1419 in^2 Fi = Sp * At ; lbf d = 0.5000 in Ab = pi() * d^2 / 4 ; in^2 q = 30 deg gg = 2 in Ac = (pi() / 16) * \ (5 * d^2 + 6 * d * gg * tan(q) + gg^2 * tan(q)^2) ; in^2 r = Ab / (Ab + Ac) # (c) Fp = 0.07 * Fmax ; lbf sa = Fp * Kf / At ; ksi END solve(error1, Fmax) # Example 10.7 n = 12 d = 250 mm pmax = 5.0 Mpa Fc = pmax * pi() * d^2 / 4 ; kN F1 = Fc / n ; kN gg = 1 mm Ab = 1 mm^2 E1 = 100 Mpa L1 = gg / 2 ; mm A1 = 5 * Ab ; mm^2 k1 = A1 * E1 / L1 ; kN/mm E2 = 70 Mpa L2 = gg / 2 ; mm A2 = 5 * Ab ; mm^2 k2 = A2 * E2 / L2 ; kN/mm kc = k1 * k2 / (k1 + k2) ; kN/mm Eb = 200 Mpa Lb = gg ; mm kb = Ab * Eb / Lb ; kN/mm DF = kb * F1 / (kb + kc) ; kN Fa = DF / 2 ; kN Sy = 69.0 MPa At = Fa / Sy ; mm^2 Aact = 58.0 mm^2 Sp = 0.6 GPa Fc = 0.55 * Sp * Aact ; kN Fp = Fc - (F1 - DF) ; kN # Homework Problems: TBD