PARSING NASA THERMODYNAMIC DATA AND USING MATLAB

CENTRIFUGAL PUMP FLOW ANALYSIS This project is all about simulating the flow through centrifugal pump. For this a typical centrifugal pump is been designed in Soidworks CAD software. The design and geometry of the centrifugal pump is not exactly as the design of the original pump, but is good enough to get the desired…

SIMULATION OF FLOW THROUGH FLOWBENCH AIM Grid dependence test  Simulation is to be done at three different levels of grid refinements at a particular valve lift. And comparing the results for the best grid refinement level     2. Effect of valve lift on mass flow rate Once decided the best grid, Parametric…

SIMULATION OF FLOW THROUGH FLOWBENCH AIM Grid dependence test  Simulation is to be done at three different levels of grid refinements at a particular valve lift. And comparing the results for the best grid refinement level     2. Effect of valve lift on mass flow rate Once decided the best grid, Parametric…

SIMULATING A FLOW OVER AN AIRFOIL In this report a flow over an airfoil is been simulated at different angle of attack.  Our main aim was to determine the drag force and the lifting force on the airfoil at different angle of attack. Simulation was done usng solidworks flow simulation. Firstly the airfoil data base…

 SIMULATION OF THE FLOW OF AIR OVER CYLINDER This project is about simulating the flow over a cylinder at different reynolds number. In this project a cylinder of 0.04 m diameter is created using solidworks CAD software and then the flow simulation is done over it. Simulation is done with two cases  Base line…

INTRODUCTION This project was all about simulating the velocity of flow of water inside a pipe. In this project a pipe was created using solid works CAD software and then the flow inside the pipe was simulated using solidworks flow simulation. The pipe created was a hollow pipe having diameter of 40 mm and inside diameter…

REPORT ON PARSING NASA THERMODYNAMIC DATA   INTRODUCTION This project is all about reading the NASA thermodynamic data and then calculatimg the thermodynamic properties (Specific heat, Enthalpy, Entropy and Molar mass) of the different species. Also to plot the graph (Temperature VS specific heat, Temperature VS Enthalpy,…

power=[100 200 300]; time=[20 30 40]; work=power.*time plot(work,time,\'color\',\'g\') xlabel(\'WORK\');ylabel(\'TIME\');

REPORT ON PARSING NASA THERMODYNAMIC DATA   INTRODUCTION This project is all about reading the NASA thermodynamic data and then calculatimg the thermodynamic properties (Specific heat, Enthalpy, Entropy and Molar mass) of the different species. Also to plot the graph (Temperature VS specific heat, Temperature VS Enthalpy,…

 Answer to what is Genetic Alogrithm Genetic Alogrith i would is simply a method used for finding a problems based on the theory of natural selection and evolutionary biology.  A genetic algorithm makes uses of techniques inspired from evolutionary biology such as selection, mutation, inheritance and recombination…

Here is a program for curve fitting using MATLAB. In this program our main motive was to write a program to predict the values of specific heat with respect to temperature And secondly to determine how we can get the minium error while curve fitting. MINIMIZING ERROR There can be two ways through which we can minimize…

Program to Sove 2nd order diffrential equation   Here we have solved the second order diffrential equation for studying the motion pendulum using MATLAB. Here I have first converted the second order diffrential equation into first order and then solved the equation using MATLAB. In the program   g = gravity…

Otto Cycle programm and PV diagram clear all close all clc %otto cycle %inputs p1=101325; t1=500; t3=2300; gamma=1.4; %engine parameters bore=0.1; stroke=0.1; cr=12; con_rod=0.15; v_s=pi/4*bore^2*stroke; v_c=v_s/(cr-1); v1=v_s+v_c; constant_c=p1*v1^gamma; v_comp=engine_kinematics(bore,stroke,cr,con_rod,180,0); p_comp=constant_c./v_comp.^gamma;…

%FLOW OVER A BYCYCLE %velocity vs drag force clear all close all clc %INPUTS %DRAG FORCE COEFFICIENT cd=0.4; %DENSITY rho=1.22; %AREA m^2 A=0.5; %VELOCITY m^3 v=[1 1.5 2 2.5 3]; %DRAG FORCE drag_force = 0.5*rho*A*v.^2*cd %plotting plot(v,drag_force) xlabel(\'Velocity\') ylabel(\'Drag Force\') grid on   %FLOW OVER…

%FORWARD KINEMATICS OF 2R ROBOTIC ARM clear all close all clc %input l1=1; l2=0.5; theta1=linspace(0,90,10); theta2=linspace(0,90,10); ct=1; %looping for i=1:length(theta1) THETA1=theta1(i); for j=1:length(theta2); THETA2=theta2(j); %coordinate x0=0; y0=0; x1=l1*cosd(THETA1); y1=l1*sind(THETA1); x2=x1+l2*cosd(THETA2);…