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On this site you can download homework solutions on: Mathematics, Physics, Chemistry, Programming C/C++, Matlab, Simulink, Electronics, Numerical Simulations, OpenCV, OpenGL and many more.


You can also inquire about special orders to resolve, please ask for our prices: downloadhomework10@gmail.com


University of Cambridge, University of Derby, Coventry University, Northumbria University, University of East London, University of Southern Queensland, University of Wollongong, Swansea University, University of Liverpool, University of Bolton, National Autonomous University of Mexico, Cardiff University.

Tuesday, 13 May 2014

Lane Emden Equation

レーンエムデン方程式

Lane Emden方程
 
We have solved the Lane Emden Equation using several numerical methods such as, 4th order Runge-Kutta, Euler scheme, or improve Euler scheme.

Please ask for any of those numerical methods or download this ready to go numerical problem.

The solution is written in matlab script, C/C++ Language, or if you want in the classic Fortran Language.



Click on BUY NOW button to download the Lane_Emden_RK4.f95 code and buy our numerical simulation.

Monday, 6 January 2014

Convolution - Matlab worked example.

We have worked the convolution of the signals x(t) and h(t):



                                                         Figure 1: It shows the signal x(t).


                                       Figure 2: It shows the impulse response of the system, h(t).

We have solved the convolution problem above, step-by-step. We have used MATLAB to solve this integral, we have included the numerical and analytical solution:

                Figure 4: It shows the common area between both functions.






                Figure 6: convolution process between two functions.

Click on BUY NOW...

Monday, 2 September 2013

Pressure amplitude distribution: Horn equation.

The pressure amplitude distribution p(x) of harmonic oscillation, p(x,t) = p(x) cos(wt), in the horn is governed by the equation:


where A(x) is the cross-section are, k is the wavenumber, w=2 pi f is de angular frequency, c = 340 m/s is the sound speed in air, f is the frequency.

Boundary conditions of horn opened at the both sides are: p(0) = p(L)=0.


It shows the first three modes of the second order differential equation given above. It shows clearly the pressure null at ends.

It shows the first 10 modes.

Click on BUY NOW, we have solved the horn equation, step-by-step. We have used MATLAB to solve this equation, we included the code.

RLC series circuit

For the circuit shown find an equation which shows how the current varies with time. Assume zero initial conditions when the switch is closed. Use Laplace transform and Kirchhoff's voltage law:



Click on BUY NOW to see the step-by-step solution, we have plotted the solution with MATLAB.


Sunday, 1 September 2013

Signal and System Analysis


It shows the continuous signal as blue line, whereas the red line is the low-pass filter signal with a cutoff frequency of 75 Hz.


It shows the continuous signal as blue line, whereas the red line is when the low-pass filter has been applied. It has a cutoff frequency of 30 Hz.

We have the step-by-step solution of Frequency Modulate and Amplitude Modulate problems... click on BUY  NOW to get the final solution.

Saturday, 31 August 2013

Cosmic Microwave Background and Point sources at mm wavelength.


We show a 10x10 sq deg map of the CMB, beam size = 10 arcmin.




A map 2x2 deg^2  CMB + point sources at 220 GHz, beam size = 1.5 arcmin.



This is my own WORK. Prohibited its reproduction.



Friday, 30 August 2013

Optimisation Methods and Simulation

Consider the minimization problem

There is not any constraint on x1 and x2.




We have solve the above problem using Simulated Annealing algorithm, with my own code and MATLAB in-built function, click on BUY NOW to see the step-by-step solution and many more.

Pressure distribution around an airfoil

Theoretical calculations for NACA 23012

Thin Airfoil Theory

Introduction


An airfoil is defined by first drawing a “mean” camber line. The straight line that joins the leading and trailing ends of the mean camber line is called the chord line. The length of the chord line is called chord, and given the symbol ‘c’.To the mean camber line, a thickness distribution is added in a direction normal to the camber line to produce the final airfoil shape. Equal amounts of thickness are added above the camber line, and below the camber line.


                                                                                (a)


                                                                                (b)

The solid blue line represents thin airfoil theory for Cp vs x/c, a) The solid red line is at AOA = 5 deg, b) The solid red line is at AOA = 10 deg.


We have an extensive analysis of pressure distribution around an airfoil, click on BUY NOW... MATLAB code is included.

Wednesday, 28 August 2013

Control Systems

What is the importance of Pole-zero diagrams in control systems?


What is the importance of Laplace Transformation in control systems?


Solve the differential equation system using MATLAB and analytically using Laplace Transform.

at t=0, x=4, y = 2 and x' = 0 and y' = 0.


We have the step by step solution and many more... 
click on BUY NOW to see the procedure.



Tuesday, 27 August 2013

Block Reduction Method


Reduce the following block diagram using Block Reduction Method and obtain the overall transfer function




We have obtained step by step the equivalent transfer function....
click on BUY NOW to see the procedure.