Week 4 - Genetic Algorithm

  FINAL INDEPENDENT PROJECT heavy vehicle drag force Aim : Model the flow over a air in the heavy vehicle for the angle of attack 55,50,45,40,35 Compare drag force.  Introduction: this project is give the result of drag force in the wind-shield-angle against to air flow .In our country I observe that…

  Centrifugal pump design and analysis Aim : In this Project, creating a 3D model of a Centrifugal pump,run a baseline flow simulation where inlet flow takes place and then perform a parametric study for different velocities and Obtain the relationship between Pressure ratio and mass flow rate. Introduction : Centrifugal…

Modelling and simulation of flow through a flowbench Aim : To create project of 3D model of flow bench and run flow analysis. And obtain a plot of lift vs mass flow rate. Introduction : Grid dependence test is also called as mesh dependence test in which the model is subjected to successive smaller cell sizes for calculations,…

Flow over a cylinder Aim : To simulate flow over a cylinder at different Reynolds number. Run a baseline simulation and then calculate the Reynolds number. Introduction : The present study to analyse the fluid flow over a cylinder and calculate Reynold's number for baseline simulation and increase the calculated…

  Flow over an airfoil Aim : Model the flow over a NACA0017 Airfoil for the angle of attack 0,2,4,6,8,10 Compare the lift anddrag force. Introduction : The NACA Airfoil are Airfoil shapes for aircraft wings developed by the National Advisory Committee for Aeronautics (NACA).…

  MBD Simulation on IC Engine Valve Train   Aim :  Model the parts and assemble and simulation on IC Engine Valve Train and Run the simulation using the below parameters Sl.No CAM Lift (mm) Speed (RPM)  Material  1 3.5 1500 Cast Carbon Steel 2 6 1500 Cast Carbon Steel   and obtain…

  MBD Simulation on a Piston Assembly Aim : the analysis of the reciprocating motion of the piston is studied for various positions of the wrist pin axis with respect to the axis of rotation of the crank. there are three conditions Sl.No Wrist Pin Offset ` Crank Speed (Rpm) 1 "0" mm 2000 2 10 mm Positive …

  Planetary Gear Aim : Use the following inputs for designing the Planetary Gear Ring Gear Module                                =2.5 (You must use the metric system in design modeler) Number of teeth         …

Internal Geneva Mechanism   AIM: simulate the internal geneva mechanism for the given condition and plot the graph  for respective condition. Contact force (between driving and the driven wheel) as a function of time. Angular Displacement of the driven wheel. INTRODUCTION: The Geneva drive is a gear…

                                                  AIR-WATER COOLED COOLER                                    STUDY…

Create a Rankine Cycle Simulator using OCTAVE/MATLAB. procedure : The given inputs are entered. Using the XSteam table and the thermodynamic equations the various state varibles such as Pressurs,Temperarture,Enthalpy and Entropy are calculated. The Net work done(W_net),Back Work Ratio and Thermal Efficiency of thr system…

   Write a function that extracts the 14 co-efficients and calculates the enthalpy, entropy and specific heats for all the species in the data file. You will be reading this file Report: 1) Firstly, the NASA Thermodynamic Data 'Thermo.dat' file was read by using fopen command.  2) Then to navigate through…

  main program: clear all close all clc x = linspace(0, 0.6, 100); y = linspace(0, 0.6, 100); [xx yy] = meshgrid(x, y); f = zeros(100); %f = get_stalagmite(x,y); for i = 1:length(xx) for j = 1:length(yy) input_vector(1) = xx(i,j); input_vector(2) = yy(i,j); f(i,j) = stalagmite(input_vector); end end option = optimoptions('ga');…

% Animates the motion of a simple pendulum as a function of time. % video link https://youtu.be/lsJZ9EYKn1Y clear all close all clc; m=1; l=1; g=9.81; t=20; c=0.05; tStep=0.1; iterations=t/tStep; % total number of iterations % pre-allocation of variables for speed theta=zeros(iterations,1); omega=zeros(iterations,1); alpha=zeros(iterations,1);…