TKWNT+5 =v #1 :n :s b :c Bedford-Fowler Example 9.2, 3rd Ed. #3 :n ì :v .4 :s i :c coefficient of friction #4 :n m :v 100 :s i :u kg :d kg :c chest mass #5 :n W :v 981 :s o :u N :d N :c weight of chest #6 :n b :v 1 :s i :u m :d m :c base width #7 :n slip :v 'left :s i :c assumed impending slip: 'none, 'left, 'right #8 :n tip :v 'left :s i :c assumed impending tip: 'none, 'left, 'right #9 :n N :v 981 :s o :u N :d N :c total normal reaction force (guess if not none) #10 :n f :v 392.4 :s o :u N :d N :c total friction force, + to right #11 :n f_max :v 392.4 :s o :u N :d N :c maximum static friction force #12 :n status :v 'impending :s o :c no slip/tip, impending, or dynamic #13 :n F :v 392.4 :s o :u N :d N :c applied force #14 :n h :v 1.25 :s o :u m :d m :c height to force F #16 :n h_LL :v 1.25 :s o :u m :d m :c analytic tip-slide-left height #17 :n g :v 9.810000000000001 :s i :u m/sec^2 :d m/sec^2 :c gravitational constant #18 :n f_A :v 392.4 :s o :u N :d N :c base friction #19 :n f_B :v 0 :s o :u N :d N :c base friction #20 :n N_A :v 981 :s o :u N :d N :c normal force #21 :n N_B :v 0 :s o :u N :d N :c normal force =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 mm :m 1000 :t um #8 :f in :m 2.5399999999999 :t cm #9 :f ft :m 12 :t in #10 :f mile :m 5280 :t ft #11 :f in :m 1000000 :t uin #12 :f 1/mm :m 25.4 :t 1/in #13 :f 1/cm :m 2.54 :t 1/in #14 :f 1/m :m .254 :t 1/in #15 :c area #16 :f in^2 :m 645.1626 :t mm^2 #17 :f m^2 :m 1000000 :t mm^2 #18 :f cm^2 :m 100 :t mm^2 #19 :f ft^2 :m 144 :t in^2 #20 :c volume #21 :f in^3 :m 16387.1623 :t mm^3 #22 :f ft^3 :m 1728 :t in^3 #23 :f m^3 :m 1E9 :t mm^3 #24 :f cm^3 :m 1000 :t mm^3 #25 :f cm^3 :t cc #26 :c force #27 :f lb :m 4.44822 :t N #28 :f N :m 100000 :t dyne #29 :f ton :m 2000 :t lb #30 :f kips :m 1000 :t lb #31 :f lb :t lbf #32 :f lb :t lbm #33 :c moments and energy #34 :f in-lb :m .1138 :t N-m #35 :f ft-lb :m 12 :t in-lb #36 :f N-m :m 100 :t N-cm #37 :f N-m :m 1000 :t N-mm #38 :f N-m :m 8.850744000000001 :t in-lb #39 :f N-m :m .7375620000000001 :t ft-lb #40 :f lb-in :t in-lb #41 :f N-m :t m-N #42 :f N-cm :t cm-N #43 :f N-m :t joule #44 :f joules :t joule #45 :f joule :t J #46 :c pressure and stress #47 :f bar :m 100000 :t Pa #48 :f psi :m 6894.757 :t Pa #49 :f MPa :m 1000000 :t Pa #50 :f MPa :t Mpa #51 :f GPa :m 1000 :t MPa #52 :f GPa :t Gpa #53 :f Pa :t pa #54 :f N/m^2 :t Pa #55 :f N/mm^2 :t MPa #56 :f N/mm^2 :m 1000000 :t N/m^2 #57 :f N/cm^2 :m 10000 :t N/m^2 #58 :f kpsi :m 1000 :t psi #59 :f psi :m 144 :t psf #60 :f kpsi :t ksi #61 :f psig :t psi :a 14.7 #62 :c acceleration #63 :f in/sec^2 :m 2.5399999999999 :t cm/sec^2 #64 :f m/sec^2 :m 100 :t cm/sec^2 #65 :f m/sec^2 :m 1000 :t mm/sec^2 #66 :f m/s^2 :t m/sec^2 #67 :f ft/sec^2 :m 12 :t in/sec^2 #68 :f ft/s^2 :t ft/sec^2 #69 :f G :m 32.17 :t ft/sec^2 #70 :c velocity #71 :f in/sec :m 2.5399999999999 :t cm/sec #72 :f m/sec :m 100 :t cm/sec #73 :f m/sec :m 1000 :t mm/sec #74 :f m/s :t m/sec #75 :f ft/sec :m 12 :t in/sec #76 :f ft/s :t ft/sec #77 :f in/s :t in/sec #78 :f rad/sec :m 9.549296584 :t rpm #79 :f mph :m 1.466666666666667 :t ft/sec #80 :c mass #81 :f blob :m 386 :t lb #82 :f slug :m 32.17 :t lb #83 :f kg :m 2.204623 :t lb #84 :f kg :m 1000 :t g #85 :f kg :m 9.806649999999999 :t N #86 :c mass mom of inertia #87 :f lb-in-sec^2 :m .1138 :t N-m-sec^2 #88 :f N-m-sec^2 :t kg-m^2 #89 :f lb-in-sec^2 :t lb-in-s^2 #90 :f blob-in^2 :t lb-in-s^2 #91 :f N-m-sec^2 :t N-m-s^2 #92 :c area moment of inertia #93 :f in^4 :m 416231.4256 :t mm^4 #94 :f m^4 :m 1E12 :t mm^4 #95 :f m^4 :m 1E8 :t cm^4 #96 :f ft^4 :m 20736 :t in^4 #97 :f in^4 :m .0000004162314256 :t m^4 #98 :c density #99 :f lb/in^3 :m 27.6805 :t g/cc #100 :f g/cc :m .001 :t g/mm^3 #101 :f lb/ft^3 :m 1728 :t lb/in^3 #102 :f kg/m^3 :m .000001 :t g/mm^3 #103 :f lb/in^3 :m .002590673575129534 :t blob/in^3 #104 :f blob/in^3 :m .08333333333333333 :t slug/in^3 #105 :f slug/ft^3 :m 1728 :t slug/in^3 #106 :f kg/mm^3 :m 1000 :t g/mm^3 #107 :f SG :t g/cc #108 :c spring rate #109 :f lb/in :m 175.126 :t N/m #110 :f N/mm :m 1000 :t N/m #111 :f lb/ft :m .08333333333333333 :t lb/in #112 :c angles #113 :f radians :m 57.29577951308232 :t degrees :c #114 :f rad :m 57.2957795129 :t deg #115 :f rev :m 360 :t deg #116 :f rad :t radian #117 :c temperature #118 :f C :m 1.8 :t F :a 32 #119 :f F :t R :a 459.69 #120 :f C :t K :a 273.16 #121 :c power #122 :f HP :m 550 :t ft-lb/sec #123 :f ft-lb/sec :m 60 :t ft-lb/min #124 :f ft-lb/sec :m 12 :t in-lb/sec #125 :f HP :m 745.699 :t watts #126 :f kw :m 1000 :t watts #127 :f HP :t hp #128 :f N-m/sec :m 8.850756136188998 :t in-lb/sec #129 :f N-m/sec :t watts #130 :f watt :t watts #131 :c flow #132 :f cfm :m 1728 :t cim #133 :c percent #134 :f dec% :m 100 :t % #136 :c fracture mechanics #137 :f MPa-m^.5 :m .909 :t ksi-in^.5 :c stress intensity #138 :f MPa-m^.5 :m 1000000 :t Pa-m^.5 :c stress intensity #139 :f ksi-in^.5 :m 1000 :t psi-in^.5 :c stress intensity #140 :f kpsi-in^.5 :m 1000 :t psi-in^.5 :c stress intensity #142 :c frequency #143 :f 1/sec :m 60 :t 1/min #144 :f Hz :t 1/sec #145 :f Hz :t hz #146 :c time #147 :f min :m 60 :t sec #148 :f hr :m 60 :t min #149 :f day :m 24 :t hr #150 :f week :m 7 :t day #151 :f year :m 52 :t week #152 :f year :m 12 :t month #153 :c viscosity #154 :f reyn :t lb-sec/in^2 :c absolute #155 :f reyn :m 6894.696003767111 :t Pa-s #156 :f reyn :m 1000000 :t ureyn #157 :f Pa-s :m 1000 :t mPa-s #158 :f cP :t mPa-s #159 :c kinematic #160 :f m^2/sec :m 10000 :t cm^2/sec #161 :f cm^2/sec :t stoke #162 :f stoke :m 100 :t cS #163 :f m^2/sec :m 1549.996853506387 :t in^2/sec #164 :c stress intensity #165 :f psi-in^.5 :m 1098.843447385385 :t Pa-m^.5 #166 :f ksi-in^.5 :m 1000 :t psi-in^.5 #167 :f MPa-m^.5 :m 1000000 :t Pa-m^.5 =l =f =r #1 :r ; Bedford-Fowler Example 9.2, 3rd Ed. :s C #3 :r ; friction and tip properties and their status :s C #4 :r f_max = ì * abs (N) #5 :r if not (known ('status)) then status = "no slip/tip" #6 :r if (or (abs (f) = f_max, N_A = 0, N_B = 0)) then status = "impending" #7 :r if (or (abs (f) > f_max, N_A < 0, N_B < 0)) then status = "dynamic" #9 :r ; Equilibrium, x-axis parallel to the plane :s C #10 :r N = N_A + N_B #11 :r f = f_A + f_B #12 :r f - F = 0 ; Ó F_x = 0 #13 :r N - W = 0 ; Ó F_y = 0 #14 :r F * h - W * b/2 + N_B * b = 0 ; Ó M_A = 0 #16 :r W = m * g ; Gravity #18 :r ; assumed slip behaviour to be checked against status :s C #19 :r if slip = "right" then f_A = - ì * abs (N_A) #20 :r if slip = "right" then f_B = - ì * abs (N_B) #21 :r if slip = "left" then f_A = ì * abs (N_A) #22 :r if slip = "left" then f_B = ì * abs (N_B) #23 :r if not (given ('slip) ) then slip = "none" #25 :r ; assumed tip behaviour to be checked against status :s C #26 :r if tip = "right" then N_A = 0 #27 :r if tip = "right" then f_A = 0 #28 :r if tip = "left" then N_B = 0 #29 :r if tip = "left" then f_B = 0 #30 :r if not (given ('tip) ) then tip = "none" #32 :r ; analytic solution inpending tip-slide to left :s C #33 :r h_LL = 0.5 * b / ì =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,24,2,0,1,0 %Or,f,35,1,0,1,0 %Xl,f,0,0,0,2,0,88,88,647,494,320,849,-1,-1,0,0,4,-1,0,0,2,-13,700,34,0,0,0,161,Arial Unicode MS,4,10,21,31,98 %Xp,f,0,0,0,2,0,110,110,669,516,480,849,-1,-1,0,0,5,-1,0,0,2,-13,700,34,0,0,0,161,Arial Unicode MS,3,13,25,99 %Xt,f,0,0,0,2,0,132,132,691,538,640,849,-1,-1,0,0,6,-1,0,0,2,-13,700,34,0,0,0,161,Arial Unicode MS,2,15,100 %Xn,f,0,0,0,2,0,154,154,713,560,800,849,-1,-1,0,0,7,-1,0,0,2,-13,700,34,0,0,0,161,Arial Unicode MS,2,15,100 %Xc,f,0,0,0,2,0,176,176,735,582,0,825,-1,-1,0,0,8,-1,0,0,2,-13,700,34,0,0,0,161,Arial Unicode MS,3,15,22,99 %Xu,f,53,3,0,2,0,22,29,1015,693,160,849,0,0,0,0,3,-1,0,0,2,-13,700,34,0,0,0,161,Arial Unicode MS,5,10,20,34,48,96 %Xf,f,0,0,0,2,0,0,0,993,664,0,849,0,0,0,0,2,-1,0,0,2,-13,700,34,0,0,0,161,Arial Unicode MS,4,16,26,38,98 %Xm,f,0,0,0,0,0,154,203,1147,867,160,825,0,0,0,0,9,-1,0,0,2,0,0,0,0,0,0,0,,0 %Xv,f,24,2,0,2,0,542,0,1084,849,-1,-1,-4,-23,0,0,0,-1,0,0,1,-13,700,34,0,0,0,161,Arial Unicode MS,6,6,11,17,27,35,86 %Xr,f,35,1,0,2,0,0,0,542,849,-1,-1,-4,-23,2,0,1,-1,0,0,3,-13,700,34,0,0,0,161,Arial Unicode MS,2,9,103 \G,0,960,1344,1,-1,-1 \G,0,1920,1344,1,-1,-1 \C,0,1920,0,0,3