ATTENTION:
BEFORE YOU READ THE ABSTRACT OR CHAPTER ONE OF THE PROJECT TOPICS BELOW, PLEASE READ THE INFORMATION BELOW.THANK YOU!
INFORMATION:
YOU CAN GET THE COMPLETE PROJECT OF THE TOPIC BELOW. THE FULL PROJECT COST N5,000 ONLY. THE FULL INFORMATION ON HOW TO PAY AND GET THE COMPLETE PROJECT IS AT THE BOTTOM OF THIS PAGE. OR
YOU CAN CALL: 08068231953, 08137701720, 09070569307, 08154275408
WHATSAPP US ON: 08137701720
ADVANCED PROPELLER DESIGN
CHAPTER ONE
INTRODUCTION
BACKGROUND OF THE STUDY
This thesis investigates aerodynamic design and analysis of UAV propeller in order to achieve improved thrust at higher speed over a wider operating range. The use of composite design will be employed to modify the stiffness properties of the propeller for a given geometry, providing blade deflections which result in improved aerodynamic characteristics. Optimization will be made with specific reference to the flight characteristics, with possible applications to similar aerospace-propellers. Preliminary calculations will be conducted to determine the optimal blade geometry using conventional blade element theories, along with a literature review of previous works and related topics. Initial analysis will involve analytical calculations based on the blade element theory with some initial inputs. Using those calculations a propeller is modeled and flow analysis is done for the validation and verification of analytical techniques.
All through the improvement of the controlled flight as we probably am aware it, each airplane require some sort of gadget to change over motor energy to some type of push. About the greater part of the early handy flying machine outlines utilized propellers to make push.
STATEMENT OF THE PROBLEM
A propeller is a pivoting airfoil which comprises of at least two sharp edges appended to a focal center point that is mounted on the motor crankshaft. The capacity of propeller is to change over motor energy to valuable push. Propeller cutting edges have a main edge, trailing edge, tip, shank, confront and a back. Propellers change over revolving movement from cylinder motors, turboprops or electric engines to give the propulsive power. They might be settled or a variable pitch. The propeller is normally appended to crankshaft of a cylinder motor, either specifically or through lessening unit. Light air ship motors frequently don’t require many-sided quality of adapting, however on bigger motors and turboprop air ship it is basic.
OBJECTIVES OF THE STUDY
- To understand the impact of advanced propeller design on improved performance of automotives
- To understand the recent challenges faced by current models of propellers
- To understand the relationship between efficient performance and an improvewment in propeller designs
RESEARCH QUESTIONS
- What is the impact of advanced propeller design on improved performance of automotives
- What are the recent challenges faced by current models of propellers
- What is the relationship between efficient performance and an improvement in propeller designs
RESEARCH HYPOTHESIS
H0: There is no relationship between efficient performance and an improvement in propeller designs
H1: There is a relationship between efficient performance and an improvement in propeller designs
HOW TO RECEIVE PROJECT MATERIAL (S)
After paying the appropriate amount (#5,000) into our bank Account below, send the following information to any of the numbers below
08068231953, 08137701720, 09070569307, 08154275408 (1) Your project topics
(2) Email Address
(3) Payment Name
OR you drop them on our WhatsApp, 08137701720
We will send your material(s) after we receive bank alert
BANK ACCOUNTS
Account Name: AMUTAH DANIEL CHUKWUDI
Account Number: 0046579864
Bank: GTBank.
OR
Account Name: AMUTAH DANIEL CHUKWUDI
Account Number: 3139283609
Bank: FIRST BANK
FOR MORE INFORMATION, CALL:
08068231953, 08137701720, 09070569307, 08154275408