The Delta Wing Is a unique type of wing platform that has been part of the aviation engineering industry for many years. The Delta Wing has been used for numerous reasons. When working with delta wings‚ engineers must know that the design has both advantages and disadvantages. Through out the assignment‚ I will be using the research I have collected to identify the range of basic scientific principles and techniques relevant to the Delta Wing design and the history behind the Delta Wing. The
Premium Wing Aerodynamics Wing design
Coefficient of lift. To achieve the overall result of the lift to drag ratio of the Piper Saratoga‚ first it is necessary to calculate the coefficient of lift 〖(C〗_L). To begin this process‚ the total weight of the aircraft needs to be calculated. With the passengers loaded and the remaining fuel on board‚ the Piper Saratoga weighed 3‚311 pounds. Next‚ the non-standard density of the air at 5‚000 MSL feet must be calculated. In order to do this‚ non-standard pressure at 5‚000 feet MSL must first
Premium Aerodynamics Force Lift
Air Resistance Lab G Luhman‚ Mary …. Abstract: The acceleration of objects dropped from about 2 meters was found in order to derive the Reynolds Number. The effect of changing weight‚ shape‚ and radius of the objects (balloons) were tested independently such that it would be clear under what criteria either laminar or turbulent air flow is prevalent. • Introduction The difference between two models‚ laminar and turbulent‚ of air resistance may seem trivial the difference is can be seen
Premium Reynolds number Fluid dynamics Aerodynamics
TABLE OF CONTENT NO. | CONTENT | PAGE | 1. | Title | 2 | 2. | Theory | 2 | 3. | Introduction | 2 | 4. | Objective | 3 | 5. | Apparatus | 3 | 6. | Procedure | 4 | 7. | Result | 6 | 8. | Calculation | 10 | 9. | Discussion | 13 | 10. | Conclusion | 14 | 11. | References | 14 | TITLE: H1 – Osborne Reynolds Demonstration INTRODUCTION: Osborne Reynold’s Demonstration has been designed for students experiment on the laminar‚ transition and turbulent flow. It consists of a transparent
Free Fluid dynamics Reynolds number Viscosity
JetBlue and WestJet: A Tale of Two IS Projects How important is the reservation system at airlines such as West Jet and JetBlue. How does it impact operational activities and decision making? Over the past years‚ it seems customers have heavily relied on airline reservation systems to book their tickets‚ reserve seats‚ pay for the tickets‚ and check-in-online. This has been very convenient for customers to plan their trips. These systems have also allowed the airlines to manage their whole flight
Premium Airline Low-cost carrier Aircraft
How do biomechanical understandings influence the learning of and performance in surfing? Problem: The problem with my surfing is my paddling technique. Understanding the fundamental relationships in mechanics‚ helps form a foundation for the analysis of human movement in surfing. The main principle or law of motion I am going to look into is Newton’s Law of Action and Reaction. This law of motion is mainly applied when paddling. It helps me understand how the application of force to my arm
Premium Force Drag Lift
Relationship between a model and Similitude For a model‚ similitude is achieved when testing conditions are created such that the test results are applicable to the real design. There are some criteria that are required to achieve similitude; 1. Geometric similarity – The model is the same shape as the application (they are usually scaled). 2. Kinematic similarity – Fluid flow of both the model and real application must undergo similar time rates of change motions. (Fluid streamlines are similar)
Free Fluid dynamics Aerodynamics Fluid mechanics
Brandon Foster MAE466 2/8/12 HW#2 1) I think about 1000 radial stations are required for a converged calculation. 2) The first plot is of a rotor with linear twist showing the lift coefficient variation with rbar in hover. The second plot is the lift coefficient max along the radius which looks to be about 1.2. The maximum thrust of the rotor in hover in terms of thrust coefficient is 0.0183. Cpo = 2.5668e-004 Cpi = 0.0020 Cpt = 0.0022 Cpideal = 0.0017 Fig Mer =
Premium Airfoil Aerodynamics MATLAB
HARDWARE 3.1 INTRODUCTION Quadcopter is a flying vehicle with six degrees of freedom which uses four rotors to push air downwards and to create a thrust force for keeping the quadcopter on the air. The pilot or flight control unit will control the orientation and tile of the multicopter by reading the data from the sensors. Gyro‚ accelerometer‚ magnetometer or GPS can be used to sense the tile‚ orientation and position of the vehicle. It can be used in many applications merely by changing the sensors
Premium Aerodynamics Lift Wing
Grade 12 Term 3 Student Name: _______________________ ID#: ________________ Student Name: _______________________ ID#: ________________ Section: _____ 2012 2013 OBJECTIVES This project will involve students in: solving real world problems with the use of Trigonometric Identities (sum and difference of angles identities‚ double angle and half angle identities). evaluating limits algebraically. Task 1: COMMUNICATION Radio waves that pass through the same place at the same time
Premium Aerodynamics