Abstract The presented project report attempts to provide a comprehensive study and develop a script for Forward kinematics motion of Robot arm Manipulator using GNU Octave. GNU Octave is software featuring a high-level programming language, primarily intended for numerical computations. Octave helps in solving linear…
Abhishek kumar
updated on 10 Apr 2020
Project Details
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Read more Projects by Abhishek kumar (9)
Solving Second order differential equations using MATLAB
Introduction The presented project report attempts to provide a comprehensive study and develop a script for solving second order differential equations for the transient motion using MATLAB. MATLAB is software featuring a high-level programming language, primarily intended for numerical computations. Octave helps in solving…
13 Feb 2021 07:30 AM IST
Stalagmite function using MATLAB
Genetic Algorithm “Select The Best, Discard The Rest” The genetic algorithm repeatedly modifies a population of individual solutions. At each step, the genetic algorithm selects individuals at random from the current population to be parents and uses them to produce the children for the next generation. The…
05 Feb 2021 01:14 PM IST
NASA thermodynamic data parsing using MATLAB
Challenge = data file parsing Aim = To write script for data parsing thermodynamic properties like specific heat, enthalpy, entropy and Molecular weight. Introduction: NASA released file which contains thermodynamic data of 53 species which can be used to calculate thermodynamic properties like entropy, enthalpy…
05 Feb 2021 01:14 PM IST
Analysis of centrifugal pump design at different velocity of impeller. Map pressure ratio and mass flow rate using flow simulation tool.
Introduction: Presented project work is focused on the analysis of centrifugal pump design. Objective: To Plot relation between pressure ratio and mass flow rate. Project work: Modelling of Centrifugal pump- 1. Start a new part file, Change unit system into the MKS system. 2. Select Top plane and select sketch, Draw two…
10 Apr 2020 02:57 PM IST
Flow Simulation through pipe using line probes at 85%, 90% and 95% for velocity profile comparision with reynolds number of 100, 1000 and 10000.
Abstract: The presented experimental work provides insight for computational fluid dynamics simulation through the pipe for velocity profile Comparision using Dassault system software package Solidworks. Flow simulation enables users to simulate a wide variety of liquids and gases for different engineering…
10 Apr 2020 02:57 PM IST
Forward Kinematics of Robotic arm manipulator
Abstract The presented project report attempts to provide a comprehensive study and develop a script for Forward kinematics motion of Robot arm Manipulator using GNU Octave. GNU Octave is software featuring a high-level programming language, primarily intended for numerical computations. Octave helps in solving linear…
10 Apr 2020 02:55 PM IST
Transient flow simulation of flow over a cylinder at different Reynolds numbers
Objective: Calculate the baseline case Reynolds number. Re = rho*U_inlet*D/mu D = cylinder diameter mu = dynamic viscosity rho = density Run a baseline simulation and then calculate the Reynolds number. Then increase the Reynolds number by a factor of 20%, 40%, and 100% then run the transient flow simulation.…
10 Apr 2020 02:55 PM IST
Modelling and simulation of flow through a Internal combustion engine cylinder valve to analyse the effect of Valve lift and mass flow rate
Study: Presented experimental work is aim towards analysing the effect of valve lift and mass flow rate in the internal combustion engine cylinder. Valve in the engine cylinder is used for the flow of gasoline in the engine cylinder. Our main focused is towards simulating the effects of valve lift and mass flow rate. Task…
10 Apr 2020 02:55 PM IST
Simulation and Modelling of NACA0017 airfoil to calculate lift and drag force at different angle of attacks i.e; 0,2,4,6,8,10.
Presented study, aims to provide detailed information about Simulation and Modelling of NACA0017 airfoil to calculate lift and drag force at different angle of attacks. The NACA airfoils are airfoil shapes for aircraft wings developed by the National Advisory Committee for Aeronautics (NACA).…
10 Apr 2020 02:55 PM IST