Added(A)/Deleted(D) following books

 A  Basic_Electronics_by_Rakesh_Kumar_Garg,_Ashish_Dixit_&_Paban_Yadav/chapter1.ipynb
A  Basic_Electronics_by_Rakesh_Kumar_Garg,_Ashish_Dixit_&_Paban_Yadav/chapter2.ipynb
A  Basic_Electronics_by_Rakesh_Kumar_Garg,_Ashish_Dixit_&_Paban_Yadav/chapter3.ipynb
A  Basic_Electronics_by_Rakesh_Kumar_Garg,_Ashish_Dixit_&_Paban_Yadav/chapter4.ipynb
A  Basic_Electronics_by_Rakesh_Kumar_Garg,_Ashish_Dixit_&_Paban_Yadav/chapter5.ipynb
A  Basic_Electronics_by_Rakesh_Kumar_Garg,_Ashish_Dixit_&_Paban_Yadav/chapter6.ipynb
A  Basic_Electronics_by_Rakesh_Kumar_Garg,_Ashish_Dixit_&_Paban_Yadav/chapter7.ipynb
A  Basic_Electronics_by_Rakesh_Kumar_Garg,_Ashish_Dixit_&_Paban_Yadav/chapter8.ipynb
A  Basic_Electronics_by_Rakesh_Kumar_Garg,_Ashish_Dixit_&_Paban_Yadav/screenshots/DCLOADLINEchapter4.png
A  Basic_Electronics_by_Rakesh_Kumar_Garg,_Ashish_Dixit_&_Paban_Yadav/screenshots/DCLOADLineCH4.png
A  Basic_Electronics_by_Rakesh_Kumar_Garg,_Ashish_Dixit_&_Paban_Yadav/screenshots/TransferCharofnchmosfetCH8.png
A  Engineering_Mechanics_by_A._K._Tayal/Chapter10.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter12.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter13.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter14.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter15.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter16.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter17.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter18.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter19.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter2.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter20.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter21.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter22.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter23.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter24.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter25.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter26.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter3.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter4.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter5.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter6.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter7.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter8.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/Chapter9.ipynb
A  Engineering_Mechanics_by_A._K._Tayal/screenshots/1.png
A  Engineering_Mechanics_by_A._K._Tayal/screenshots/2.png
A  Engineering_Mechanics_by_A._K._Tayal/screenshots/3.png
A  Semiconductor_circuit_approximations_by_A.P._Malvino/ch10.ipynb
A  Semiconductor_circuit_approximations_by_A.P._Malvino/ch11.ipynb
A  Semiconductor_circuit_approximations_by_A.P._Malvino/ch12.ipynb
A  Semiconductor_circuit_approximations_by_A.P._Malvino/ch14.ipynb
A  Semiconductor_circuit_approximations_by_A.P._Malvino/ch16.ipynb
A  Semiconductor_circuit_approximations_by_A.P._Malvino/ch2.ipynb
A  Semiconductor_circuit_approximations_by_A.P._Malvino/ch3.ipynb
A  Semiconductor_circuit_approximations_by_A.P._Malvino/ch4.ipynb
A  Semiconductor_circuit_approximations_by_A.P._Malvino/ch5.ipynb
A  Semiconductor_circuit_approximations_by_A.P._Malvino/ch6.ipynb
A  Semiconductor_circuit_approximations_by_A.P._Malvino/ch7.ipynb
A  Semiconductor_circuit_approximations_by_A.P._Malvino/ch8.ipynb
A  Semiconductor_circuit_approximations_by_A.P._Malvino/ch9.ipynb
A  Semiconductor_circuit_approximations_by_A.P._Malvino/screenshots/ACloadLineChapter10.png
A  Semiconductor_circuit_approximations_by_A.P._Malvino/screenshots/DCandACloadlinechapter9.png
A  Semiconductor_circuit_approximations_by_A.P._Malvino/screenshots/Powerratingchapter9.png

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diff --git a/Engineering_Mechanics_by_A._K._Tayal/Chapter20.ipynb b/Engineering_Mechanics_by_A._K._Tayal/Chapter20.ipynb
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+{
+ "cells": [
+  {
+   "cell_type": "markdown",
+   "metadata": {},
+   "source": [
+    "# Chapter 20 Motion of Projectile"
+   ]
+  },
+  {
+   "cell_type": "markdown",
+   "metadata": {},
+   "source": [
+    "# Example 20.1 Motion of Projectile"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": 4,
+   "metadata": {
+    "collapsed": false
+   },
+   "outputs": [
+    {
+     "name": "stdout",
+     "output_type": "stream",
+     "text": [
+      "The velocity of the projectile is 435.272891 m/s\n",
+      "The direction of the projectile is 5.841405 degree\n"
+     ]
+    }
+   ],
+   "source": [
+    "import math\n",
+    "# Initilization of variables\n",
+    "v_o=500 # m/s # velocity of the projectile\n",
+    "alpha=30 # angle at which the projectile is fired\n",
+    "t=30 # seconds\n",
+    "g=9.81 # m/s**2 # acc due to gravity\n",
+    "# Calculations\n",
+    "v_x=v_o*(math.cos(alpha*math.pi/180)) # m/s # Initial velocity in the horizontal direction\n",
+    "v_y=v_o*(math.sin(alpha*math.pi/180)) # m/s # Initial velocity in the vertical direction\n",
+    "# MOTION IN HORIZONTA DIRECTION:\n",
+    "V_x=v_x # m/s # V_x=Horizontal velocity after 30 seconds\n",
+    "# MOTION IN VERTICAL DIRECTION: # using the eq'n v=u+a*t\n",
+    "V_y=v_y-(g*t) # m/s # -ve sign denotes downward motion\n",
+    "# Let the Resultant velocity be v_R. It is given as,\n",
+    "v_R=math.sqrt((V_x)**2+(-V_y)**2) # m/s\n",
+    "theta=math.degrees(math.atan((-V_y)/V_x)) # degree # direction of the projectile\n",
+    "# Results\n",
+    "print('The velocity of the projectile is %f m/s'%v_R) \n",
+    "# The answer of velocity is wrong in the text book.\n",
+    "print('The direction of the projectile is %f degree'%theta)"
+   ]
+  },
+  {
+   "cell_type": "markdown",
+   "metadata": {},
+   "source": [
+    "# Example 20.2 Motion of Projectile"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": 5,
+   "metadata": {
+    "collapsed": false
+   },
+   "outputs": [
+    {
+     "name": "stdout",
+     "output_type": "stream",
+     "text": [
+      "(a) The velocity of body B for horizontal range is 9.306049 m/s\n",
+      "(b) The velocity of body B for the maximum height is 12.247449 m/s\n",
+      "(c) The velocity of body B for equal time of flight is 12.247449 m/s\n"
+     ]
+    }
+   ],
+   "source": [
+    "# Initilization of variables\n",
+    "v_A=10 # m/s # velocity of body A\n",
+    "alpha_A=60 # degree # direction of body A\n",
+    "alpha_B=45 # degree # direction of body B\n",
+    "# Calculations\n",
+    "# (a) The velocity (v_B) for the same range is given by eq'n;\n",
+    "v_B=math.sqrt((v_A**2*math.sin(2*alpha_A*math.pi/180))/(math.sin(2*alpha_B*math.pi/180))) # m/s\n",
+    "# (b) Now velocity v_B for the same maximum height is given as,\n",
+    "v_b=math.sqrt((v_A**2)*((math.sin(alpha_A*math.pi/180))**2/(math.sin(alpha_B*math.pi/180))**2)) # m/s\n",
+    "# (c) Now the velocity (v) for the equal time of flight is;\n",
+    "v=(v_A*math.sin(alpha_A*math.pi/180))/(math.sin(alpha_B*math.pi/180)) # m/s\n",
+    "# Results\n",
+    "print('(a) The velocity of body B for horizontal range is %f m/s'%v_B)\n",
+    "print('(b) The velocity of body B for the maximum height is %f m/s'%v_b)\n",
+    "print('(c) The velocity of body B for equal time of flight is %f m/s'%v)"
+   ]
+  },
+  {
+   "cell_type": "markdown",
+   "metadata": {},
+   "source": [
+    "# Example 20.3 Motion of Projectile"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": 6,
+   "metadata": {
+    "collapsed": false
+   },
+   "outputs": [
+    {
+     "name": "stdout",
+     "output_type": "stream",
+     "text": [
+      "The least velocity with which the ball can be thrown is 9.779954 m/s\n",
+      "The angle of projection for the same is 60.255119 degree\n"
+     ]
+    }
+   ],
+   "source": [
+    "# Initilization of variables\n",
+    "y=3.6 # m # height of the wall\n",
+    "x_1=4.8 # m # position of the boy w.r.t the wall\n",
+    "x_2=3.6 # m # distance from the wall where the ball hits the ground\n",
+    "g=9.81 # m/s**2 # acc due to gravity\n",
+    "# Calculations\n",
+    "# The range of the projectile is r, given as,\n",
+    "r=x_1+x_2 # m\n",
+    "# Let the angle of the projection be alpha, which is derived and given as,\n",
+    "alpha=math.degrees(math.atan((y)/(x_1-(x_1**2/r)))) # degree\n",
+    "# Now substuting the value of alpha in eq'n 3 we get the least velocity (v_o) as;\n",
+    "v_o=math.sqrt((g*r)/(math.sin(2*alpha*math.pi/180))) # m/s\n",
+    "# Results\n",
+    "print('The least velocity with which the ball can be thrown is %f m/s'%v_o)\n",
+    "print('The angle of projection for the same is %f degree'%alpha)"
+   ]
+  },
+  {
+   "cell_type": "markdown",
+   "metadata": {},
+   "source": [
+    "# Example 20.5 Motion of Projectile"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": 23,
+   "metadata": {
+    "collapsed": false
+   },
+   "outputs": [
+    {
+     "name": "stdout",
+     "output_type": "stream",
+     "text": [
+      "The time difference between the two hits is 67.908579 seconds\n"
+     ]
+    }
+   ],
+   "source": [
+    "# Initilization of variables\n",
+    "v_o=400 # m/s # initial velocity of each gun\n",
+    "r=5000 # m # range of each of the guns\n",
+    "g=9.81 # m/s**2 # acc due to gravity\n",
+    "pi=180 # degree \n",
+    "# Calculations\n",
+    "# now from eq'n 1\n",
+    "theta_1=math.degrees(math.asin((r*g)/(v_o**2)))/(2) \n",
+    "# from eq'n 3\n",
+    "theta_2=(pi-(2*theta_1))/2 # degree \n",
+    "# For 1st & 2nd gun, s is\n",
+    "s=r # m\n",
+    "# For 1st gun \n",
+    "v_x=v_o*math.cos(theta_1*math.pi/180) # m/s\n",
+    "# Now the time of flight for 1st gun is t_1, which is given by relation,\n",
+    "t_1=s/(v_x) # seconds\n",
+    "# For 2nd gun\n",
+    "V_x=v_o*math.cos(theta_2*math.pi/180)\n",
+    "# Now the time of flight for 2nd gun is t_2\n",
+    "t_2=s/(V_x) # seconds\n",
+    "# Let the time difference between the two hits be delta.T. Then,\n",
+    "deltaT=t_2-t_1 # seconds\n",
+    "# Results\n",
+    "print('The time difference between the two hits is %f seconds'%deltaT)"
+   ]
+  },
+  {
+   "cell_type": "markdown",
+   "metadata": {},
+   "source": [
+    "# Example 20.6 Motion of Projectile"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": 24,
+   "metadata": {
+    "collapsed": false
+   },
+   "outputs": [
+    {
+     "name": "stdout",
+     "output_type": "stream",
+     "text": [
+      "The pilot should release the bomb from a distance of 3028.912664 m\n",
+      "The angle at which the target would appear is 33.436901 degree\n"
+     ]
+    }
+   ],
+   "source": [
+    "# Initilization of variables\n",
+    "h=2000 # m/ height of the plane\n",
+    "v=540*(1000/3600) # m/s # velocity of the plane\n",
+    "g=9.81 # m/s**2 # acc due to gravity\n",
+    "# Calculations\n",
+    "# Time t required to travel down a height 2000 m is given by eq'n,\n",
+    "u=0 # m/s # initial velocity\n",
+    "t=math.sqrt((2*h)/(g)) # seconds\n",
+    "# Now let s be the horizonta distance travelled by the bomb in time t seconds, then\n",
+    "s=v*t # m\n",
+    "# angle is given as theta,\n",
+    "theta=math.degrees(math.atan(h/s)) # degree\n",
+    "# Results\n",
+    "print('The pilot should release the bomb from a distance of %f m'%s)\n",
+    "print('The angle at which the target would appear is %f degree'%theta)"
+   ]
+  },
+  {
+   "cell_type": "markdown",
+   "metadata": {},
+   "source": [
+    "# Example 20.7 Motion of Projectile"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": 25,
+   "metadata": {
+    "collapsed": false
+   },
+   "outputs": [
+    {
+     "name": "stdout",
+     "output_type": "stream",
+     "text": [
+      "(a) The maximum height to which the bullet will rise above the soldier is 127.420999 m\n",
+      "(b) The velocity with which the bullet will hit the target is 104.790267 m/s\n",
+      "(c) The time required to hit the target is 11.111111 seconds\n"
+     ]
+    }
+   ],
+   "source": [
+    "# Initilization of variables\n",
+    "theta=30 # degree # angle at which the bullet is fired\n",
+    "s=-50 # position of target below hill\n",
+    "v=100 # m/s # velocity at which the bullet if fired\n",
+    "g=9.81 # m/s**2 \n",
+    "# Calculations\n",
+    "v_x=v*math.cos(theta*math.pi/180) # m/s # Initial velocity in horizontal direction\n",
+    "v_y=v*math.sin(theta*math.pi/180) # m/s # Initial velocity in vertical direction\n",
+    "# (a) Max height attained by the bullet\n",
+    "h=v_y**2/(2*g) # m\n",
+    "# (b)Let the vertical Velocity with which the bullet will hit the target be V_y. Then,\n",
+    "V_y=math.sqrt((2*-9.81*s)+(v_y)**2) # m/s # the value of V_y is +ve & -ve\n",
+    "# Let V be the velocity with wich it hits the target\n",
+    "V=math.sqrt((v_x)**2+(V_y)**2) # m/s\n",
+    "# (c) The time required to hit the target\n",
+    "a=g # m/s**2\n",
+    "t=(v_y-(-V_y))/a # seconds\n",
+    "# Results\n",
+    "print('(a) The maximum height to which the bullet will rise above the soldier is %f m'%h)\n",
+    "print('(b) The velocity with which the bullet will hit the target is %f m/s'%V)\n",
+    "print('(c) The time required to hit the target is %f seconds'%t)"
+   ]
+  },
+  {
+   "cell_type": "markdown",
+   "metadata": {},
+   "source": [
+    "# Example 20.8 Motion of Projectile"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": 26,
+   "metadata": {
+    "collapsed": false
+   },
+   "outputs": [
+    {
+     "name": "stdout",
+     "output_type": "stream",
+     "text": [
+      "The distance x where the hammer hits the round is 5.159708 m\n"
+     ]
+    }
+   ],
+   "source": [
+    "# Initilization of variables\n",
+    "W=30 # N # Weight of the hammer\n",
+    "theta=30 # degree # ref fig.20.12\n",
+    "mu=0.18 # coefficient of friction\n",
+    "s=10 # m # distance travelled by the hammer # fig 20.12\n",
+    "g=9.81 # m/s**2 # acc due to gravity\n",
+    "# Calculations\n",
+    "# The acceleration of the hammer is given as,\n",
+    "a=g*((math.sin(theta*math.pi/180))-(mu*math.cos(theta*math.pi/180))) # m/s**2\n",
+    "# The velocity of the hammer at point B is,\n",
+    "v=math.sqrt(2*a*s) # m/s\n",
+    "# Let the initial velocity of the hammer in horizontal direction be v_x & v_y in vertical direction, Then,\n",
+    "v_x=v*math.cos(theta*math.pi/180) # m/s\n",
+    "v_y=v*math.sin(theta*math.pi/180) # m/s\n",
+    "# MOTION IN VERTICAL DIRECTION\n",
+    "# Now, let time required to travel vertical distance (i.e BB'=S=5 m) is given by finding the roots of the second degree eq'n as,\n",
+    "# From the eq'n 4.9*t**2+4.1*t-5=0,\n",
+    "a=4.9\n",
+    "b=4.1\n",
+    "c=-5\n",
+    "# The roots of the eq'n are,\n",
+    "t=((-b)+(math.sqrt(b**2-(4*a*c))))/(2*a)\n",
+    "# MOTION IN HORIZONTAL DIRECTION\n",
+    "# Let the horizotal distance travelled by the hammer in time t be s_x.Then,\n",
+    "s_x=v_x*math.cos(theta*math.pi/180)*t # m\n",
+    "x=1+s_x # m\n",
+    "# Results\n",
+    "print('The distance x where the hammer hits the round is %f m'%x)"
+   ]
+  },
+  {
+   "cell_type": "markdown",
+   "metadata": {},
+   "source": [
+    "# Example 20.9 Motion of Projectile"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": 27,
+   "metadata": {
+    "collapsed": false
+   },
+   "outputs": [
+    {
+     "name": "stdout",
+     "output_type": "stream",
+     "text": [
+      "(a) The velocity of shell just before bursting is 500.255037 m/s\n",
+      "(b) The velocity of first part immediately after the shell burst is 1000.510074 m/s\n",
+      "(c) The velocity of second part immediately after the shell burst is 1000.510074 m/s\n",
+      "(b) The distance between the firing point & the point where the second part of the shell hit the ground is 3000.000000 m\n"
+     ]
+    }
+   ],
+   "source": [
+    "# Initilization of variables\n",
+    "s=1000 # m # distance OB (ref fig.20.13)\n",
+    "h=19.6 # m # height of shell from ground\n",
+    "g=9.81 # m/s**2 # acc due to gravity\n",
+    "# Calculations\n",
+    "# MOTION OF ENTIRE SHELL FROM O to A.\n",
+    "v_y=math.sqrt(2*(g)*h) # m/s # initial velocity of shell in vertical direction\n",
+    "t=v_y/g # seconds # time taken by the entire shell to reach point A\n",
+    "v_x=s/t # m/s # velocity of shell in vertical direction\n",
+    "# VELOCITIES OF THE TWO PARTS OF THE SHELL AFTER BURSTING AT A:\n",
+    "# Let v_x2 be the horizontal velocity of 1st & the 2nd part after bursting which is given as,\n",
+    "v_x2=v_x*2 # m/s\n",
+    "# Now distance BC travelled by part 2 is\n",
+    "BC=v_x2*t # m\n",
+    "# Distance from firing point OC\n",
+    "OC=s+BC # m\n",
+    "# Results\n",
+    "print('(a) The velocity of shell just before bursting is %f m/s'%v_x)\n",
+    "print('(b) The velocity of first part immediately after the shell burst is %f m/s'%v_x2)\n",
+    "print('(c) The velocity of second part immediately after the shell burst is %f m/s'%v_x2)\n",
+    "print('(b) The distance between the firing point & the point where the second part of the shell hit the ground is %f m'%OC)"
+   ]
+  },
+  {
+   "cell_type": "markdown",
+   "metadata": {},
+   "source": [
+    "# Example 20.10 Motion of Projectile"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": 33,
+   "metadata": {
+    "collapsed": false
+   },
+   "outputs": [
+    {
+     "name": "stdout",
+     "output_type": "stream",
+     "text": [
+      "The range covered (i.e BC) is 7650.920998 m\n"
+     ]
+    }
+   ],
+   "source": [
+    "# Initilization of variables\n",
+    "v_o=200 # m/s # initial velocity\n",
+    "theta=60 # degree # angle of the incline\n",
+    "y=5 # rise of incline\n",
+    "x=12 # length of incline\n",
+    "g=9.81 # m/s**2 # acc due to gravity\n",
+    "# Calculations\n",
+    "# The angle of the inclined plane with respect to horizontal\n",
+    "beta=math.degrees(math.atan(y/x)) # degree\n",
+    "# The angle of projection with respect to horizontal\n",
+    "alpha=90-theta # degree\n",
+    "# Range is given by eq'n (ref. fig.20.14)\n",
+    "AB=(2*v_o**2*(math.sin((alpha-beta)*math.pi/180))*math.cos(alpha*math.pi/180))/(g*(math.cos(beta*math.pi/180))**2) # m\n",
+    "# Range AC when the short is fired down the plane\n",
+    "AC=(2*v_o**2*(math.sin((alpha+beta)*math.pi/180))*math.cos(alpha*math.pi/180))/(g*(math.cos(beta*math.pi/180))**2) # m\n",
+    "BC=AB+AC # m\n",
+    "# Results\n",
+    "print('The range covered (i.e BC) is %f m'%BC)"
+   ]
+  }
+ ],
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