Curve Fitting For Linear Quadratic and Cubic Polynomial Using Python

Radar Mast and Yacht Assembly  Google Drive Link, Feature Tree & Image's / View's 1) Radar Mast Google Drive Link https://drive.google.com/file/d/11tEpuayYw-QiRHnkePmd9XP3YsllpUoL/view?usp=sharing Radar Mast Feature Tree Featrure_Tree_1 Featrure_Tree_2 Featrure_Tree_3 Featrure_Tree_4 Featrure_Tree_5   Radar Mast Image's…

Report  Title: Design, Assembly and Photo – Realistic Rendering of an American Predator Yacht Objective: To Design every individual component of the yacht with suitable appearances. To assemble all parts of the yacht in the appropriate position with proper mates. Rendering the fully assembled Sunseeker Predator…

OBJECTIVE The main objective of this project is to obtain sustainable knowledge in SOLIDWORK part modeling, SOLIDWORK assembly and rendering through, 1) Modelling each part of the American chopper with proper Dimensions and appearance using the SOLIDWORKS part. 2) Assembling all the parts of the American chopper using…

Objective: - To write a python program in order to perform curve fitting. The curve fit is used to know the mathematical nature of data. Curve fitting is the process of constructing a curve, or mathematical functions, which possess the closest proximity to the real series of data. By curve fitting, we can mathematically…

Aim:- To Plot PV Diagram for the Otto Cycle and Computing Thermal Efficiency Objective: Obtain Values of Pressure and Volume of 4 Points in the Graph. Making an equation for the Isentropic Compression and Expansion Process. Obtaining Thermal Efficiency. Introduction:- This cycle consists of the two reversible adiabatic…

File Parsing of NASAs Thermodynamic Data Using Matlab AIM:-  To parse the NASA thermodynamic properties data file and introduce the required properties. OBJECTIVES:- To extract the 14 coefficients and to calculate the enthalpy, entropy, and specific heats for all the species in the data file. Calculate the molecular…

  % solving_2nd_order_ODE clear all close all clc % inputs % Damping coefficent (N*Sec/M) b = 0.05; % Gravity (M/sec^2) g = 9.81; % Length (M) l = 1; % Mass (kg) m = 1; % initial condition % Angular Displacement (rad) and Angular Velocity (rad/sec) Angular_Displacement = 0; Angular_Velocity = 3; theta_0 = [0;3]; %…