# Example 15.1 MKS(deg, N) m0 = 100 kg f = 200 N q = 45 deg delt = 10 s v2 = f * delt * cos(q) / m0 nc = (m0 * grav() * delt - f * delt * sin(q)) / delt # Example 15.2 FPS(deg) q = 30 deg cp0 = 20 lb / (1 s) delt = 2 s v1 = 3 ft/s mu = 0.3 w0 = 50 lb m0 = w0 / grav() BEGIN v2 = 1 m/s nc = 1 N e1 = m0 * v1 + cp0 * delt^2 / 2 - mu * nc * delt + w0 * delt * sin(q) - m0 * v2 e2 = nc - w0 * cos(q) END solve(e1,e2,v2,nc) # Example 15.3 MKS(deg, N) ma = 3 kg mb = 5 kg delt = 6 s BEGIN va = 1 m/s vb = -2 * va tb = 1 N ta = 2 * tb e1 = -2 * tb * delt + ma * grav() * delt - ma * va e2 = mb * grav() * delt - tb * delt - mb * vb END solve(e1,e2,va,tb) # Example 15.4 MKS(deg, kN) ma = 15e3 kg mb = 12e3 kg va = 1.5 m/s vb = 0.75 m/s v2 = (ma * va - mb * vb) / (ma + mb) delt = 0.8 s fav = ma * (v2 - va) / delt # Example 15.5 FPS(kip) wc = 1200 lb mc = wc / grav() wp = 8 lb mp = wp / grav() v = 1500 ft/s delt = 0.03 s v2 = v * mp / mc fave = mp * v / delt # Example 15.6 MKS() mt = 350e3 kg mb = 50e3 kg vt1 = 3 m/s vt2 = mt * vt1 / (mt + mb) # Example 15.7 MKS() mp = 800 kg mh = 300 kg y0 = 0.5 m v = sqrt(mh * grav() * y0 / (0.5 * mh)) v2 = mh * v / (mh + mp) ii = mh * v - mh * v2 # Example 15.8 MKS() mb = 40 kg mt = 15 kg x = 2 m ss = 2 * mb / (mb + mt) # Example 15.9 FPS() w1 = 6 lb m1 = w1 / grav() w2 = 18 lb m2 = w2 / grav() e = 0.5 r = 3 ft va1 = sqrt(w1 * r/ (0.5 * m1)) BEGIN va2 = 1 m/s vb2 = 1 m/s e1 = m1 * va1 - m2 * vb2 - m1 * va2 e2 = (vb2 - va2) / (va1) - e END solve(e1,e2,va2,vb2) # Example 15.10 m0 = 1.5 kg x0 = 1 m delx = 0.25 m k = 800 N/m e = 0.8 y0 = x0 + delx BEGIN vb1 = 1 m/s u1 = -y0 * grav() * m0 + 0.5 * k * delx^2 - 0.5 * m0 * vb1^2 END solve(u1,vb1) BEGIN vb2 = 1 m/s u2 = vb2 / (-vb1) - e END solve(u2,vb2) BEGIN s3 = 0.2 m u3 = 0.5 * m0 * vb2^2 - (-m0 * grav() * (x0 + s3) + 0.5 * k * s3^2) END solve(u3,s3) # Example 15.11 MKS(deg) ma = 1 kg va = 3 m/s qa = 30 deg mb = 2 kg vb = 1 m/s qb = 45 deg e = 0.75 va1 = PolarVec(va, qa) vb1 = -PolarVec(vb, qb) BEGIN vax2 = 1 m/s vbx2 = 1 m/s e1 = ma * va1[1] + mb * vb1[1] - (ma * vax2 + mb * vbx2) e2 = (vbx2 - vax2) / (va1[1] - vb1[1]) - 1 END solve(e1,e2,vax2,vbx2) # Example 15.13 p = 10 N r = 0.4 m m0 = 5 kg cm0 = 3 N m / (1 s) delt = 4 s va = (r * p * delt + cm0 * delt^2 / 2) / (m0 * r) # Example 15.14 FPS w0 = 0.8 lb m0 = w0 / grav() r1 = 1.75 ft v1 = 4 ft/s vc = 6 ft/s r2 = 6 ft v2 = v1 * r1 / r2 v20 = sqrt(v2^2 + vc^2) uf = 0.5 * m0 * v20^2 - 0.5 * m0 * v1^2 # Example 15.15 MKS m0 = 2 kg k = 20 N/m vd1 = 1.5 m/s x = 0.2 m x0 = 0.5 m vd2 = vd1 * x0 / (x0 + x) BEGIN vd3 = 1 m/s e = 0.5 * m0 * vd1^2 - (0.5 * m0 * vd3^2 + 0.5 * k * x^2) END solve(e,vd3) sqrt(vd3^2 - vd2^2) # Example 15.16 MKS(kN) rho = 1000 kg/m^3 pa = 100 kPa q = 0.2 m^3 / s me = 20 kg ab = pi() * (5 cm)^2 aa = pi() * (10 cm)^2 dmdt = rho * q vb = q / ab va = q / aa fa = pa * aa fx = fa - dmdt * (-va) fy = -me * grav() - dmdt * (-vb) M0 = dmdt * (0.3 m * vb) - me * grav() * 0.125 m # Example 15.17 FPS d = 2 in vw = 25 ft/s vblade = 5 ft/s gw = 62.4 lb/ft^3 dmdt = gw / grav() * (vw - vblade) * pi() * d^2 / 4 f = dmdt * (vw - vblade) p = f * vblade; hp # Homework Problems: TBD