Merge pull request #13 from rcc02007/master

Update

lecture_22/01_phugoid/01_01_Phugoid_Theory.ipynb

@@ -33,7 +33,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 1,
+   "execution_count": 2,
    "metadata": {
     "collapsed": false
    },
@@ -53,10 +53,10 @@
        "        "
       ],
       "text/plain": [
-       "<IPython.lib.display.YouTubeVideo at 0x7f514c38ffd0>"
+       "<IPython.lib.display.YouTubeVideo at 0x7fef9c611a50>"
       ]
      },
-     "execution_count": 1,
+     "execution_count": 2,
      "metadata": {},
      "output_type": "execute_result"
     }

lecture_23/.ipynb_checkpoints/lecture_23-checkpoint.ipynb

@@ -0,0 +1,6 @@
+{
+ "cells": [],
+ "metadata": {},
+ "nbformat": 4,
+ "nbformat_minor": 2
+}

lecture_23/boussinesq_lookup.m

@@ -0,0 +1,32 @@
+function sigma_z=boussinesq_lookup(q,a,b,z)
+  % function that determines stress under corner of an a by b rectangular platform
+  % z-meters below the platform. The calculated solutions are in the fmn data
+  % m=fmn(:,1)
+  % in column 2, fmn(:,2), n=1.2
+  % in column 3, fmn(:,2), n=1.4
+  % in column 4, fmn(:,2), n=1.6
+
+  fmn= [0.1,0.02926,0.03007,0.03058
+        0.2,0.05733,0.05894,0.05994
+        0.3,0.08323,0.08561,0.08709
+        0.4,0.10631,0.10941,0.11135
+        0.5,0.12626,0.13003,0.13241
+        0.6,0.14309,0.14749,0.15027
+        0.7,0.15703,0.16199,0.16515
+        0.8,0.16843,0.17389,0.17739];
+
+  m=a/z;
+  n=b/z;
+  if n < 1.3
+      f=fmn(:,2);
+    elseif n > 1.5
+        f=fmn(:,4);
+    else
+        f=fmn(:,3);
+  end
+  [~,i_fit]=sort(abs(m-fmn(:,1)));
+  x=fmn(i_fit(1:4),1);
+  y=f(i_fit(1:4));
+  f_out = Newtint(x,y,m);
+  sigma_z=q*f_out;
+end

lecture_23/coriolis.m

@@ -0,0 +1,63 @@
+function [t,r] = coriolis(L)
+  % In class we ran this function using L=41.8084 (the latitude of Storrs, CT). This
+  % function takes the latitude (L) in degrees and mass (m) and calculates the trajectory
+  % of a particle with a 100 N load directed North. The initial conditions are set as L
+  % (in radians) * radius of Earth, 0 m/s initial x-velocity, 0 m E-W position (add to
+  % -72.261319 degrees for longitude of Storrs), 0 m/s initial E-W velocity, 10 m initial
+  % altitude, 0 m/s initial z-velocity [L*pi/180*R 0 0 0 10 0], the force is given as 100
+  % N North, 0 West and 9.81*m z (neutrally buoyant) [100 0 9.81*m]
+  %
+  % the output of myode is ddr=[dx/dt d2x/dt2 dy/dt d2y/dt2 dz/dt d2z/dt2]' and the input
+  % to myode is r=[x dx/dt y dy/dt z dz/dt]'
+  % using ode23 solver solves for r as a function of time, here we solve from 0 to 200 s
+  % r(:,1) = x (the north-south position from 0 to 200 s)
+  % r(:,3) = x (the West-East position from 0 to 200 s)
+  % r(:,5) = x (the altitude from 0 to 200 s)
+
+  % define ordinary differential equation in terms of 6 first order ODE's
+  function ddr = myode(t,r,R,L)
+    g=9.81; % acceleration due to gravity m/s^2
+    l=10; % 10 m long cable
+    we=2*pi/23.934/3600; % rotation of Earth (each day is 23.934 hours long)
+    ddr=zeros(4,1); % initialize ddr
+
+    ddr(1) = r(2); % x North(+) South (-)
+    ddr(2) = 2*we*r(4).*sin(L)-g/l*r(1); % dx/dt 
+    ddr(3) = r(4); % y West (+) East (-)
+    ddr(4) = -2*we*(r(2).*sin(L))-g/l*r(3); % dy/dt
+  end
+
+  R=6378.1e3; % radius of Earth in m
+  L=L*pi/180;
+  [t,r]=ode45(@(t,r) myode(t,r,R,L),[0 30000], [1 0 0 0 ]);
+  figure()
+  z=-sqrt(10^2-r(:,1).^2-r(:,3).^2);
+  figure(1)
+  we=2*pi/23.934/3600; % rotation of Earth (each day is 23.934 hours long)
+
+  plot(t,tan(we*sin(L)*t),t,-r(:,3)./r(:,1),'.')
+  xlabel('time (s)','Fontsize',18)
+  ylabel('-y/x','Fontsize',18)
+  % Plot Coriolis effect path
+  figure(2)
+  title('Path at 0 hr, 4.1 hrs, 8.3 hrs','Fontsize',24) 
+  N=length(t);
+  i1=[1:100]; i2=[floor(N/2):floor(N/2)+100]; i3=[N-100:N];
+  plot3(r(i1,1),r(i1,3),z(i1))
+  hold on
+  plot3(r(i2,1),r(i2,3),z(i2),'k-')
+  plot3(r(i3,1),r(i3,3),z(i3),'g-')
+  xlabel('X (m)','Fontsize',18)
+  ylabel('Y (m)','Fontsize',18)
+  zlabel('Z (m)','Fontsize',18)
+  title('Coriolis acceleration Foucalt Pendulum')
+
+%  figure()
+%  % Plot Eotvos effect for deviation upwards
+%  plot(1e-3*(r(:,1)-r(1,1)),r(:,5))
+%  xlabel('North (+km)','Fontsize',18)
+%  ylabel('Altitude (+m)','Fontsize',18)
+%  title('Eotvos effect with north force')
+%
+end
+

lecture_23/eulode.m

@@ -0,0 +1,29 @@
+function [t,y] = eulode(dydt,tspan,y0,h,varargin)
+% eulode: Euler ODE solver
+%   [t,y] = eulode(dydt,tspan,y0,h,p1,p2,...):
+%           uses Euler's method to integrate an ODE
+% input:
+%   dydt = name of the M-file that evaluates the ODE
+%   tspan = [ti, tf] where ti and tf = initial and
+%   final values of independent variable
+%   y0 = initial value of dependent variable
+%   h = step size
+%   p1,p2,... = additional parameters used by dydt
+% output:
+%   t = vector of independent variable
+%   y = vector of solution for dependent variable
+if nargin<4,error('at least 4 input arguments required'),end
+ti = tspan(1);tf = tspan(2);
+if ~(tf>ti),error('upper limit must be greater than lower'),end
+t = (ti:h:tf)'; n = length(t);
+% if necessary, add an additional value of t
+% so that range goes from t = ti to tf
+if t(n)<tf
+  t(n+1) = tf;
+  n = n+1;
+end
+y=zeros(n,length(y0));
+y(1,:)=y0;
+for i = 1:n-1 %implement Euler's method
+  y(i+1,:) = y(i,:) + dydt(t(i),y(i,:),varargin{:})'*(t(i+1)-t(i));
+end