TKWNT+5 =v #1 :n :s b :c Find equivalent static force for an impact #2 :n :s b :c Data for sample 12.5, Pytel "Mech of Materials" #5 :n m :v 80 :s i :u kg :d kg :c Mass of impacting object #6 :n W :v 784.8000000000001 :s o :u N :d N :c Weight of impacting object #7 :n h :v 10 :s i :u m :d m :c Height of vertical drop #8 :n V :v 14.0071410359145 :s o :u m/sec :d m/sec :c Speed at impact #9 :n k :v 46875 :s i :u N/m :d N/m :c Body stiffness at impact point #10 :n Ä_s :v .0167424 :s o :u m :d m :c Static deflection due to weight #11 :n Ä_max :v .5956450757217141 :s o :u m :d m :c Maximum dynamic deflection #12 :n F_static :v 27920.86292445535 :s o :u N :d N :c Equivalent static force #13 :n Factor :v 35.57704246235391 :s o :c Amplification to get static load #15 :n E :v 2E11 :s i :u N/m^2 :d MPa :c Modulus of elasticity #16 :n L :v 1.2 :s i :u m :d m :c Length of bar or beam #17 :n A :v .0018 :s o :u m^2 :d mm^2 :c Area of bar #18 :n EA :v 3.6E8 :s o :u N :d N :c Axial property (optional) #19 :n k_bar :v 3E8 :s o :u N/m :d N/m :c Stiffness of axial bar #21 :n EI :v 27000 :s o :u N_m^2 :d N_m^2 :c Bending property (optional) #22 :n I :v .000000135 :s o :u m^4 :d m^4 :c Moment of inertial of beam #23 :n k_cant :v 46875 :s o :u N/m :d N/m :c Stiffness at end of a cantilever beam #24 :n k_mid :v 750000 :s o :u N/m :d N/m :c Stiffness at middle of simple beam #25 :n k_over :s b :u N/m :d N/m :c Stiffness at overhang end of simple beam #27 :n g :v 9.810000000000001 :s i :u m/sec^2 :d m/sec^2 :c Gravitational constant #28 :n a :s b :u m :d m :c Overhang of a simple beam, L=a+b #29 :n b :s b :u m :d m :c Support span of overhanging simple beam #30 :n B :v .06 :s i :u m :d m :c Rectangle base length #31 :n H :v .03 :s i :u m :d m :c Rectangle height =u #1 :c Unit Master Sheet by R.L. Norton, #2 :c appended by J.E. Akin #4 :c length #5 :f cm :m 10 :t mm #6 :f m :m 100 :t cm #7 :f km :m 1000 :t m #8 :f mm :m 1000 :t um #9 :f in :m 2.5399999999999 :t cm #10 :f ft :m 12 :t in #11 :f mile :m 5280 :t ft #12 :f in :m 1000000 :t uin #13 :f 1/mm :m 25.4 :t 1/in #14 :f 1/cm :m 2.54 :t 1/in #15 :f 1/m :m .254 :t 1/in #16 :c area #17 :f in^2 :m 645.1626 :t mm^2 #18 :f m^2 :m 1000000 :t mm^2 #19 :f cm^2 :m 100 :t mm^2 #20 :f ft^2 :m 144 :t in^2 #21 :c volume #22 :f in^3 :m 16387.1623 :t mm^3 #23 :f ft^3 :m 1728 :t in^3 #24 :f m^3 :m 1E9 :t mm^3 #25 :f cm^3 :m 1000 :t mm^3 #26 :f cm^3 :t cc #27 :c force #28 :f lb :m 4.44822 :t N #29 :f N :m 100000 :t dyne #30 :f kN :m 1000 :t N #31 :f ton :m 2000 :t lb #32 :f kips :m 1000 :t lb #33 :f lb :t lbf #34 :f lb :t lbm #35 :c moments, work and energy #36 :f in-lb :m .1138 :t N-m #37 :f ft-lb :m 12 :t in-lb #38 :f N-m :m 100 :t N-cm #39 :f N-m :m 1000 :t N-mm #40 :f N-m :m 8.850744000000001 :t in-lb #41 :f N-m :m .7375620000000001 :t ft-lb #42 :f lb-in :t in-lb #43 :f N-m :t m-N #44 :f N-cm :t cm-N #45 :f N-m :t joule #46 :f joules :t joule #47 :f joule :t J #48 :f N-m :t kg m^2/sec^2 #50 :c pressure and stress #51 :f bar :m 100000 :t Pa #52 :f psi :m 6894.757 :t Pa #53 :f MPa :m 1000000 :t Pa #54 :f MPa :t Mpa #55 :f GPa :m 1000 :t MPa #56 :f GPa :t Gpa #57 :f Pa :t pa #58 :f N/m^2 :t Pa #59 :f N/mm^2 :t MPa #60 :f N/mm^2 :m 1000000 :t N/m^2 #61 :f N/cm^2 :m 10000 :t N/m^2 #62 :f kpsi :m 1000 :t psi #63 :f psi :m 144 :t psf #64 :f kpsi :t ksi #65 :f psig :t psi :a 14.7 #66 :c acceleration #67 :f in/sec^2 :m 2.5399999999999 :t cm/sec^2 #68 :f in/s^2 :m 2.5399999999999 :t cm/s^2 #69 :f m/sec^2 :m 100 :t cm/sec^2 #70 :f m/sec^2 :m 1000 :t mm/sec^2 #71 :f m/s^2 :t m/sec^2 #72 :f ft/sec^2 :m 12 :t in/sec^2 #73 :f ft/s^2 :t ft/sec^2 #74 :f G :m 32.17 :t ft/sec^2 #75 :c velocity #76 :f in/sec :m 2.5399999999999 :t cm/sec #77 :f m/sec :m 100 :t cm/sec #78 :f m/sec :m 1000 :t mm/sec #79 :f m/sec :m 3.280839895013253 :t ft/sec #80 :f (m/sec)^2 :m 10.76391012 :t (ft/sec)^2 #81 :f m/sec :m 39.37007874015903 :t in/sec #82 :f (m/sec)^2 :m 1550.0031 :t (in/sec)^2 #83 :f m/sec :m 3.6 :t km/hr #84 :f m/s :t m/sec #85 :f ft/sec :m 12 :t in/sec #86 :f ft/s :t ft/sec #87 :f in/s :t in/sec #88 :f rad/sec :m 9.549296584 :t rpm #89 :f mph :m 1.466666666666667 :t ft/sec #90 :c mass #91 :f blob :m 386 :t lb #92 :f slug :m 32.17 :t lb #93 :f kg :m 2.204623 :t lb #94 :f kg :m 1000 :t g #95 :f kg :m 9.806649999999999 :t N #96 :c mass mom of inertia #97 :f lb-in-sec^2 :m .1138 :t N-m-sec^2 #98 :f lb-in-s^2 :m .1138 :t N-m-s^2 #99 :f N-m-sec^2 :t kg-m^2 #100 :f N-m-s^2 :t kg-m^2 #101 :f lb-in-sec^2 :t lb-in-s^2 #102 :f blob-in^2 :t lb-in-s^2 #103 :f N-m-sec^2 :t N-m-s^2 #104 :c area moment of inertia #105 :f in^4 :m 416231.4256 :t mm^4 #106 :f m^4 :m 1E12 :t mm^4 #107 :f m^4 :m 1E8 :t cm^4 #108 :f ft^4 :m 20736 :t in^4 #109 :f in^4 :m .0000004162314256 :t m^4 #110 :c density #111 :f lb/in^3 :m 27.6805 :t g/cc #112 :f g/cc :m .001 :t g/mm^3 #113 :f lb/ft^3 :m 1728 :t lb/in^3 #114 :f kg/m^3 :m .000001 :t g/mm^3 #115 :f lb/in^3 :m .002590673575129534 :t blob/in^3 #116 :f blob/in^3 :m .08333333333333333 :t slug/in^3 #117 :f slug/ft^3 :m 1728 :t slug/in^3 #118 :f kg/mm^3 :m 1000 :t g/mm^3 #119 :f SG :t g/cc #120 :c spring rate, and line loads #121 :f lb/in :m 175.126 :t N/m #122 :f N/mm :m 1000 :t N/m #123 :f lb/ft :m .08333333333333333 :t lb/in #124 :f N/m :m .06852209266470997 :t lb/ft #125 :c angles, angular velocity & acceleration #126 :f radians :m 57.29577951308232 :t degrees :c #127 :f rad :m 57.2957795129 :t deg #128 :f rev :m 360 :t deg #129 :f rad :t radians #130 :f rad/sec :m 57.29577951308232 :t deg/sec #131 :f rad/s :m 57.29577951308232 :t deg/s #132 :f rad/sec^2 :m 57.29577951308232 :t deg/sec^2 #133 :f rad/s^2 :m 57.29577951308232 :t deg/s^2 #134 :f rad/sec :m 9.549296584 :t rpm #135 :c temperature #136 :f C :m 1.8 :t F :a 32 #137 :f F :t R :a 459.69 #138 :f C :t K :a 273.16 #139 :c power #140 :f HP :m 550 :t ft-lb/sec #141 :f HP :m 550 :t ft-lb/s #142 :f ft-lb/sec :m 60 :t ft-lb/min #143 :f ft-lb/s :m 60 :t ft-lb/min #144 :f ft-lb/sec :m 12 :t in-lb/sec #145 :f ft-lb/s :m 12 :t in-lb/s #146 :f HP :m 745.699 :t watts #147 :f kw :m 1000 :t watts #148 :f kW :m 1000 :t watts #149 :f HP :t hp #150 :f N-m/sec :m 8.850756136188998 :t in-lb/sec #151 :f N-m/s :m 8.850756136188998 :t in-lb/s #152 :f N-m/sec :t watts #153 :f N-m/s :t watts #154 :f watt :t watts #155 :f W :t watts #156 :c flow #157 :f cfm :m 1728 :t cim #158 :c percent #159 :f dec% :m 100 :t % #161 :c fracture mechanics #162 :f MPa-m^.5 :m .909 :t ksi-in^.5 :c stress intensity #163 :f MPa-m^.5 :m 1000000 :t Pa-m^.5 :c stress intensity #164 :f ksi-in^.5 :m 1000 :t psi-in^.5 :c stress intensity #165 :f kpsi-in^.5 :m 1000 :t psi-in^.5 :c stress intensity #167 :c frequency #168 :f 1/sec :m 60 :t 1/min #169 :f 1/s :m 60 :t 1/min #170 :f Hz :t 1/sec #171 :f Hz :t 1/s #172 :f Hz :t hz #173 :c time #174 :f min :m 60 :t sec #175 :f min :m 60 :t s #176 :f hr :m 60 :t min #177 :f day :m 24 :t hr #178 :f week :m 7 :t day #179 :f year :m 52 :t week #180 :f year :m 12 :t month #181 :c viscosity #182 :f reyn :t lb-sec/in^2 :c absolute #183 :f reyn :t lb-s/in^2 #184 :f reyn :m 6894.696003767111 :t Pa-s #185 :f reyn :m 1000000 :t ureyn #186 :f Pa-s :m 1000 :t mPa-s #187 :f cP :t mPa-s #188 :c kinematic #189 :f m^2/sec :m 10000 :t cm^2/sec #190 :f m^2/s :m 10000 :t cm^2/s #191 :f cm^2/sec :t stoke #192 :f cm^2/s :t stoke #193 :f stoke :m 100 :t cS #194 :f m^2/sec :m 1549.996853506387 :t in^2/sec #195 :f m^2/s :m 1549.996853506387 :t in^2/s #196 :c stress intensity #197 :f psi-in^.5 :m 1098.843447385385 :t Pa-m^.5 #198 :f ksi-in^.5 :m 1000 :t psi-in^.5 #199 :f MPa-m^.5 :m 1000000 :t Pa-m^.5 #200 :c specific heat #201 :f J/kgC :t Wsec/kgC #202 :f Wsec/kgC :m 3600 :t Whr/kgC =l =f =r #1 :r ; Static load approximation of impact load :s C #2 :r ; J.E. Akin Oct. 2011 :s C #4 :r W = m * g ; gravity #5 :r sqrt (2 * g * h) = V ; impact speed #6 :r F_static = W * Ä_max / Ä_s ; equivalent static load #7 :r W / k = Ä_s ; static deflection of massless member #8 :r Ä_max = Ä_s + sqrt (Ä_s^2 + 2*h*Ä_s) ; dynamic deflection #9 :r Ä_max = Ä_s * Factor ; scale factor #10 :r Factor = 1 + sqrt (1 + 2 * h / Ä_s) ; alternate impact factor definition #11 :r ; Bar & cantilever Fixed -------------------L------------------- W :s C #12 :r k_bar = EA / L ; stiffness at end bar of length L #13 :r k_cant = 3*EI / L^3 ; stiffness at end of cantilever #14 :r ; Mid-span Pin ------- L/2------ W -------- L/2 ------- Pin :s C #15 :r k_mid = 48 * EI / L^3 ; stiffness at middle of simple beam #16 :r ; Overhang Pin --------- b --------- Pin ----- a -------- W, L = a + b :s C #17 :r k_over = 3 * EI / (a^2 * L) ; end stiffness of overhanging simple beam #18 :r E * A = EA ; axial property #19 :r E * I = EI ; bending property #20 :r L = a + b ; overhang (a) and support span of beam #21 :r A = B * H ; rectangle area, base * height #22 :r I = B * H^3 / 12 ; rectangle moment of inertia #23 :r ; NOTE Ä_s can be computed in a FEA study by applying the load at a point, :s C #24 :r ; and solving for the displacement at that point, in the load direction, :s C =p =t =n =c =g #1 :c .000001 :i 100 :t 1 :y Yes =d :c E :f 0 :v E :g 0.000001 :i 1000 :t 100 :p 0.000001 :r 5.00 :e 0 :d 1 :s 0 :n 0 :a 0 =s :r 0 :v %Tv,f,8,1,0,1,0 %Or,f,32,1,0,1,0 %Xu,f,146,2,0,2,0,0,8,972,672,160,811,0,0,0,0,3,-1,0,0,2,-11,400,34,0,0,0,161,Arial,5,10,22,36,50,98 %Xl,f,0,0,0,2,0,88,88,649,478,320,811,-1,-1,0,0,4,-1,0,0,2,-15,700,34,0,0,0,161,Arial Unicode MS,4,10,21,31,98 %Xp,f,0,0,0,2,0,110,110,671,500,480,811,-1,-1,0,0,5,-1,0,0,2,-15,700,34,0,0,0,161,Arial Unicode MS,3,13,25,99 %Xt,f,0,0,0,2,0,132,132,693,522,640,811,-1,-1,0,0,6,-1,0,0,2,-15,700,34,0,0,0,161,Arial Unicode MS,2,15,100 %Xn,f,0,0,0,2,0,154,154,715,544,800,811,-1,-1,0,0,7,-1,0,0,2,-15,700,34,0,0,0,161,Arial Unicode MS,2,15,100 %Xc,f,0,0,0,2,0,176,176,737,566,0,787,-1,-1,0,0,8,-1,0,0,2,-15,700,34,0,0,0,161,Arial Unicode MS,3,15,22,99 %Xf,f,0,0,0,2,0,0,0,993,664,0,811,0,0,0,0,2,-1,0,0,2,-11,400,34,0,0,0,161,Arial,4,16,26,38,98 %Xm,f,0,0,0,0,0,154,203,1147,867,160,787,0,0,0,0,9,-1,0,0,2,0,0,0,0,0,0,0,,0 %Xv,f,8,1,0,2,0,6,120,1050,732,-1,-1,0,0,0,0,0,-1,0,0,1,-11,400,34,0,0,0,161,Arial,6,6,14,22,30,40,91 %Xr,f,32,1,0,2,0,0,0,1044,737,-1,-1,0,0,0,0,1,-1,0,0,1,-11,400,34,0,0,0,161,Arial,2,11,105 \G,0,960,1344,1,-1,-1 \G,0,1920,1344,1,-1,-1 \C,0,1920,0,0,3