Working code
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README.md
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README.md
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Solve the boundary layer velocity profile using a finite difference method. Directly animate the result.
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blflow.lyx
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blflow.lyx
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#LyX 2.1 created this file. For more info see http://www.lyx.org/
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\lyxformat 474
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\begin_document
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\begin_header
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\textclass article
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\use_default_options true
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\maintain_unincluded_children false
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\language english
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\language_package default
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\inputencoding auto
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\fontencoding global
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\font_roman default
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\font_sans default
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\font_typewriter default
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\font_math auto
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\font_default_family default
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\use_non_tex_fonts false
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\font_sc false
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\font_osf false
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\font_sf_scale 100
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\font_tt_scale 100
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\graphics default
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\output_sync 0
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\index_command default
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\paperfontsize default
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\use_hyperref false
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\papersize default
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\use_geometry false
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\use_package amsmath 1
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\use_package amssymb 1
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\use_package cancel 1
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\use_package esint 1
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\use_package mathdots 1
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\use_package mathtools 1
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\use_package mhchem 1
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\use_package stackrel 1
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\use_package stmaryrd 1
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\use_package undertilde 1
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\cite_engine basic
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\cite_engine_type default
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\biblio_style plain
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\use_bibtopic false
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\use_indices false
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\paperorientation portrait
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\suppress_date false
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\justification true
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\use_refstyle 1
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\index Index
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\shortcut idx
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\color #008000
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\end_index
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\secnumdepth 3
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\tocdepth 3
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\paragraph_separation indent
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\paragraph_indentation default
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\quotes_language english
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\html_be_strict false
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\end_header
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\begin_body
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\begin_layout Title
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Boundary layer flow
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\end_layout
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\begin_layout Standard
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\begin_inset Formula
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\begin{equation}
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\frac{\partial u}{\partial t}-\frac{1}{s^{2}}\frac{\partial^{2}u}{\partial y^{2}}=K(t)
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\end{equation}
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\end_inset
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\end_layout
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\begin_layout Standard
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\begin_inset Formula $y=0:u=0$
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\end_inset
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,
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\begin_inset Formula $y=1,\frac{\partial u}{\partial y}=0$
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\end_inset
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\end_layout
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\begin_layout Standard
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Discretization, FTCD:
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\end_layout
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\begin_layout Standard
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\begin_inset Formula
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\begin{equation}
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\frac{u_{i}^{n+1}-u_{i}^{n}}{\Delta t}-\frac{1}{s^{2}}\frac{u_{i+1}^{n}-2u_{i}^{n}-u_{i-1}^{n}}{\Delta y^{2}}=K^{n}
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\end{equation}
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\end_inset
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\end_layout
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\begin_layout Standard
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Rewriting:
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\begin_inset Note Note
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status open
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\begin_layout Plain Layout
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\begin_inset Formula $u_{i}^{n+1}-u_{i}^{n}-\frac{\Delta t}{\Delta y^{2}s^{2}}\frac{u_{i+1}^{n}-2u_{i}^{n}-u_{i-1}^{n}}{}=K^{n}\Delta t$
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\end_inset
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\end_layout
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\begin_layout Plain Layout
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\begin_inset Formula $u_{i}^{n+1}=\Delta tK^{n}+u_{i}^{n}+\frac{\Delta t}{\Delta y^{2}s^{2}}\left(u_{i+1}^{n}-2u_{i}^{n}-u_{i-1}^{n}\right)$
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\end_inset
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\end_layout
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\begin_layout Plain Layout
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\begin_inset Formula $u_{0}=0$
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\end_inset
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\end_layout
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\begin_layout Plain Layout
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and
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\end_layout
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\begin_layout Plain Layout
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\begin_inset Formula $u_{N}-u_{n-1}=0$
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\end_inset
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\end_layout
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\end_inset
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\end_layout
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\begin_layout Standard
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\begin_inset Formula
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\[
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\]
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\end_inset
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\end_layout
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\end_body
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\end_document
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73
blflow.py
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73
blflow.py
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#!/usr/bin/python
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# Boundary layer flow
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from numpy import *
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import time
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import matplotlib
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matplotlib.use('TkAgg')
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# from matplotlib.pylab import *
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import pylab as p
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# import matplotlib.animation as animation
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def K(t): #Forcing function
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return (1-exp(-0.1*t))*cos(t)
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s=10
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#Define domain
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n=50 #Number of gridpoints
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y=linspace(0,1,n)
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dy=y[1]-y[0]
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dt=0.0005
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l=(dt/(s**2*dy**2))
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hnu=exp(-sqrt(1j)*s*y)
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# fnu=(1-1j)/s
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fnu=0
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def u_ex(tn):
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return (((1-hnu)/(1-fnu))*exp(1j*(tn))/1j).real
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def u_np1(un,tn,dt):
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Kn=K(tn)
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unp1=un
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unp1[0]=0 #Velocity zero ver here
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for i in range(1,un.size-1):
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unp1[i]=dt*Kn+un[i]+l*(un[i-1]-2*un[i]+un[i+1])
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unp1[-1]=unp1[-2] #Approximate 'infinity' bc
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return unp1
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un0=zeros(n,float)
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t=0
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un=un0
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# un.append(un0)
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# Make the plot
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p.ion()
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linefd, = p.plot(un0,y)
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linee, = p.plot(un0,y)
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p.legend(('Finite difference','Periodic exact'))
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p.ylim(0,1)
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p.xlim(-1.5,1.5)
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p.ylabel('y')
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p.xlabel('u')
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p.grid('on')
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i=0
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uold=un
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while(True):
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t+=dt
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uold=un
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un=u_np1(uold,t,dt)
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if(i%20==0):
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linefd.set_xdata(un)
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linee.set_xdata(u_ex(t))
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p.draw()
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# print("Time:",t)
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i+=1
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