Aerodynamics Technology 10 Hour - Part 1 Student Workbook Issue: US180/10/2a-IQ-0201a. Lesson Module: 71.18/3 Written by: LJ Technical Dept
|
|
|
- Marian Ross
- 5 years ago
- Views:
Transcription
1 Aerodynamics Technology 1 Hour - Part 1 Issue: US18/1/2a-IQ-21a Copyright 24,. No part of this Publication may be adapted or reproduced in any material form, without the prior written permission of. Lesson Module: 71.18/3 Written by: LJ Technical Dept
2 Assignment 1 What is Aerodynamics? What are the four forces acting on an airplane in flight? 1) The upward force is... 2) The forward force is... 3) The backward force is... 4) The downward force is... Assignment 2 Looking at Wind Tunnels The flow of air through the wind tunnel is smooth. This type of airflow is called... airflow. The wind tunnel instrumentation measures: Assignment 3 Measuring Drag Fill in results from the drag meter calibration (Range 4). Mass Drag Meter Table 3.1 SW1.1
3 Fill in the graph using your results from Table 3.1 (Range 4). (V) RANGE RANGE RANGE RANGE 2 RANGE Graph 3.1 Complete the table to show how drag changes with facing area. Shape Width (in) Height (in) One block Two Blocks Facing Area (sq in) Drag Meter Drag Range Drag Table 3.2 A larger surface area causes... drag. (More/Less) SW1.2
4 Assignment 4 Testing Vehicle Designs Fill in the table to show drag resistance for the different automobile shapes. Car Drag Meter Drag Range Drag Station Wagon Compact Car Sports Car Table 4.1 The... vehicle shape has the lowest drag reading because.... Assignment 5 Car Building on Computer Fill in the results from the performance tests on the different automobile designs. Car Drag Coefficient Quarter Mile Top Speed (mph) Quarter Mile time lapsed (seconds) Gas Mileage (mpg) 1 2 Your Design Table 5.1 Drag coefficient tells us A high drag coefficient means A low drag coefficient means The lower the drag coefficient the... the speed and the... fuel economy (higher / lower). SW1.3
5 Aerodynamics Technology 1 Hour - Part 2 Issue: US18/1/2b-IQ-21B Copyright 25,. No part of this Publication may be adapted or reproduced in any material form, without the prior written permission of. Lesson Module: 71.18/3 Written by: LJ Technical Dept
6 Assignment 6 Introducing Lift and Aeronautics Complete the following sentence by filling in the missing words. When air travels faster, its pressure... Lift occurs when the air pressure below a wing is... than the air pressure above the wing. Assignment 7 Wings and The Angle of Attack Using a ruler, draw and label the chordline, the airflow direction and the angle of attack onto the diagram below. Diagram 7.1 Use the CAI to fill in the missing labels: Diagram SW2.1
7 Assignment 8 Measuring Lift Force Fill in results from the lift meter calibration. (Range 4) Table 8.1 Mass Lift Meter Fill in the table to show how lift changes with the angle of attack for a flat wing: Angle of Attack Table Lift Meter Lift Range Lift Force Lift... (increases/decreases) with increased angle of attack. Stall occurs when... Fill in graph 8.1 using results from Table 8.1 (Range 4) SW2.2
8 (V) RANGE RANGE RANGE 2 Assignment Graph 8.1 RANGE 1 Comparing Different Types of Wing Fill in the table using the results from the cambered wing section: Angle of Attack Table Lift Meter Lift Range Lift Force SW2.3
9 Fill in the table using the results from the symmetrical wing section: Angle of Attack Table Lift Meter Lift Range Lift Force Fill in the graph using the results from table 8.2 (of Assignment 8) and tables 9.1 and 9.2. Plot three lines on the graph, one from each table. Label each line with the wing type used. LIFT FORCE Graph ANGLE OF ATTACK (degrees) SW2.4
10 Referring to graph 9.1, complete the following statements. At zero angle of attack the... wing generates the greater lift. Which wing has a stall condition with the lowest angle of attack?... wing. Assignment 1 Problem Solving: Designing a Glider Maneuvering an Airplane Note down the different components that are used to maneuver an airplane Purpose Device used Where found (wing/tail) Slow aircraft down Adjust the pitch of the airplane Make the airplane yaw Make the airplane roll At the airport Write down what the functions of the different areas of an airport are The Apron... The Taxiway... The Runway... The Hangers... The Gate... The Control Tower... Describe how you made the glider roll:... Describe what you saw when you raised the elevator flaps:... What happened when you tried to make the glider yaw? SW2.5
11 Appendix 1 Rectangles from Assignment 1 Fold Rectangle A Rectangle B CUT FOLD SW2.6
12 Appendix 2 Wind Vane for Assignment 2 GLUE Wind Vane SW2.7
The Fly Higher Tutorial IV
The Fly Higher Tutorial IV THE SCIENCE OF FLIGHT In order for an aircraft to fly we must have two things: 1) Thrust 2) Lift Aerodynamics The Basics Representation of the balance of forces These act against
The Metric Glider. By Steven A. Bachmeyer. Aerospace Technology Education Series
The Metric Glider By Steven A. Bachmeyer Aerospace Technology Education Series 10002 Photographs and Illustrations The author wishes to acknowledge the following individuals and organizations for the photographs
BUILD AND TEST A WIND TUNNEL
LAUNCHING INTO AVIATION 9 2018 Aircraft Owners and Pilots Association. All Rights Reserved. UNIT 2 SECTION D LESSON 2 PRESENTATION BUILD AND TEST A WIND TUNNEL LEARNING OBJECTIVES By the end of this lesson,
PRE-TEST Module 2 The Principles of Flight Units /60 points
PRE-TEST Module 2 The Principles of Flight Units 1-2-3.../60 points 1 Answer the following questions. (20 p.) moving the plane (4) upward / forward. Opposed to that is 1. What are the names of the four
Exploration Series. AIRPLANE Interactive Physics Simulation Page 01
AIRPLANE ------- Interactive Physics Simulation ------- Page 01 What makes an airplane "stall"? An airplane changes its state of motion thanks to an imbalance in the four main forces acting on it: lift,
Detailed study 3.4 Topic Test Investigations: Flight
Name: Billanook College Detailed study 3.4 Topic Test Investigations: Flight Ivanhoe Girls Grammar School Questions 1 and 2 relate to the information shown in the diagram in Figure 1. z Question 1 y Figure
The Academy of Model Aeronautics ALPHA: Potential Energy Background Information for the Teacher
The Academy of Model Aeronautics ALPHA: Potential Energy Background Information for the Teacher When the rubber motor of a model plane is wound it becomes a form of stored potential energy. As the rubber
This IS A DRAG IS IT A LIFT!!!!! Aerodynamics
Problems in Technology This IS A DRAG OR IS IT A LIFT!!!!! Aerodynamics Our mission is to better understand the science and study of aerodynamics. Well, simply put aerodynamics is the way air moves around
PRINCIPLES OF FLIGHT
CHAPTER 3 PRINCIPLES OF FLIGHT INTRODUCTION Man has always wanted to fly. Legends from the very earliest times bear witness to this wish. Perhaps the most famous of these legends is the Greek myth about
Aviation Merit Badge Knowledge Check
Aviation Merit Badge Knowledge Check Name: Troop: Location: Test Score: Total: Each question is worth 2.5 points. 70% is passing Dan Beard Council Aviation Knowledge Check 1 Question 1: The upward acting
No Description Direction Source 1. Thrust
AERODYNAMICS FORCES 1. WORKING TOGETHER Actually Lift Force is not the only force working on the aircraft, during aircraft moving through the air. There are several aerodynamics forces working together
Stability and Flight Controls
Stability and Flight Controls Three Axes of Flight Longitudinal (green) Nose to tail Lateral (blue) Wing tip to Wing tip Vertical (red) Top to bottom Arm Moment Force Controls The Flight Controls Pitch
WHAT IS GLIDER? A light engineless aircraft designed to glide after being towed aloft or launched from a catapult.
GLIDER BASICS WHAT IS GLIDER? A light engineless aircraft designed to glide after being towed aloft or launched from a catapult. 2 PARTS OF GLIDER A glider can be divided into three main parts: a)fuselage
Aerodynamics Principles
Aerodynamics Principles Stage 1 Ground Lesson 3 Chapter 3 / Pages 2-18 3:00 Hrs Harold E. Calderon AGI, CFI, CFII, and MEI Lesson Objectives Become familiar with the four forces of flight, aerodynamic
XI.D. Crossed-Control Stalls
References: FAA-H-8083-3; POH/AFM Objectives Key Elements Elements Schedule Equipment IP s Actions SP s Actions Completion Standards The student should understand the dynamics of a crossed-control stall
AF101 to AF109. Subsonic Wind Tunnel Models AERODYNAMICS. A selection of optional models for use with TecQuipment s Subsonic Wind Tunnel (AF100)
Page 1 of 4 A selection of optional models for use with TecQuipment s Subsonic Wind Tunnel (AF100) Dimpled Sphere Drag Model (from AF109) shown inside the TecQuipment AF100 Wind Tunnel. Cylinder, aerofoils,
Theory of Flight Stalls. References: FTGU pages 18, 35-38
Theory of Flight 6.07 Stalls References: FTGU pages 18, 35-38 Review 1. What are the two main types of drag? 2. Is it possible to eliminate induced drag? Why or why not? 3. What is one way to increase
Ottawa Remote Control Club Wings Program
+ Ottawa Remote Control Club Wings Program Guide line By Shahram Ghorashi Chief Flying Instructor Table of Contents Rule and regulation Quiz 3 Purpose of the program 4 Theory of flight Thrust 4 Drag 4
Flight Control Systems Introduction
Flight Control Systems Introduction Dr Slide 1 Flight Control System A Flight Control System (FCS) consists of the flight control surfaces, the respective cockpit controls, connecting linkage, and necessary
II.E. Airplane Flight Controls
References: FAA-H-8083-3; FAA-8083-3-25 Objectives Key Elements Elements Schedule Equipment IP s Actions SP s Actions Completion Standards The student should develop knowledge of the elements related to
Principles of glider flight
Principles of glider flight [ Lecture 2: Control and stability ] Richard Lancaster Email: Richard@RJPLancaster.net Twitter: @RJPLancaster ASK-21 illustrations Copyright 1983 Alexander Schleicher GmbH &
Chapter 3: Aircraft Construction
Chapter 3: Aircraft Construction p. 1-3 1. Aircraft Design, Certification, and Airworthiness 1.1. Replace the letters A, B, C, and D by the appropriate name of aircraft component A: B: C: D: E: A = Empennage,
Aero Club. Introduction to Flight
Aero Club Presents Introduction to RC Modeling Module 1 Introduction to Flight Centre For Innovation IIT Madras Page2 Table of Contents Introduction:... 3 How planes fly How is lift generated?... 3 Forces
Aerodynamic Terms. Angle of attack is the angle between the relative wind and the wing chord line. [Figure 2-2] Leading edge. Upper camber.
![Aerodynamic Terms. Angle of attack is the angle between the relative wind and the wing chord line. [Figure 2-2] Leading edge. Upper camber.](/thumbs/82/86661300.jpg "Aerodynamic Terms. Angle of attack is the angle between the relative wind and the wing chord line. [Figure 2-2] Leading edge. Upper camber.")
Chapters 2 and 3 of the Pilot s Handbook of Aeronautical Knowledge (FAA-H-8083-25) apply to powered parachutes and are a prerequisite to reading this book. This chapter will focus on the aerodynamic fundamentals
CFD ANALYSIS OF FLOW AROUND AEROFOIL FOR DIFFERENT ANGLE OF ATTACKS
www.mechieprojects.com CFD ANALYSIS OF FLOW AROUND AEROFOIL FOR DIFFERENT ANGLE OF ATTACKS PRESENTATION OUTLINE AIM INTRODUCTION LITERATURE SURVEY CFD ANALYSIS OF AEROFOIL RESULTS CONCLUSIONS www.mechieprojects.com
Big News! Dick Kline Inventor of the KF AirFoil Contacts rcfoamfighters.
Big News! Dick Kline Inventor of the KF AirFoil Contacts rcfoamfighters. (Copy of Email from Dick Kline to rcfoamfighters on 3/28/09) --------------------------------------------------------------------------------
Low Speed Wind Tunnel Wing Performance
Low Speed Wind Tunnel Wing Performance ARO 101L Introduction to Aeronautics Section 01 Group 13 20 November 2015 Aerospace Engineering Department California Polytechnic University, Pomona Team Leader:
What happens to a fluid (water or air) when it moves from entering a wide opening to entering a narrow opening?
What happens to a fluid (water or air) when it moves from entering a wide opening to entering a narrow opening? The water (or air) speeds up. Since the same amount of water/air has to travel through a
Aerodynamic Forces on a Wing in a Subsonic Wind Tunnel. Learning Objectives
Aerodynamic Forces on a Wing in a Subsonic Wind Tunnel AerodynamicForces Lab -1 Learning Objectives 1. Familiarization with aerodynamic forces 2. Introduction to airfoil/wing basics 3. Use and operation
Aerodynamically Efficient Wind Turbine Blade S Arunvinthan 1, Niladri Shekhar Das 2, E Giriprasad 3 (Avionics, AISST- Amity University, India)
International Journal of Engineering Science Invention ISSN (Online): 2319 6734, ISSN (Print): 2319 6726 Volume 3 Issue 4ǁ April 2014ǁ PP.49-54 Aerodynamically Efficient Wind Turbine Blade S Arunvinthan
Subsonic wind tunnel models
aerodynamics AF1300a to AF1300l A selection of optional models for use with TecQuipment s Subsonic Wind Tunnel (AF1300) Dimpled Sphere Drag Model (from AF1300j) shown inside the TecQuipment AF1300 Wind
A Different Approach to Teaching Engine-Out Glides
A ifferent Approach to Teaching Engine-Out Glides es Glatt, Ph., ATP/CFI-AI, AGI/IGI When student pilots begin to learn about emergency procedures, the concept of the engine-out glide is introduced. The
C-1: Aerodynamics of Airfoils 1 C-2: Aerodynamics of Airfoils 2 C-3: Panel Methods C-4: Thin Airfoil Theory
ROAD MAP... AE301 Aerodynamics I UNIT C: 2-D Airfoils C-1: Aerodynamics of Airfoils 1 C-2: Aerodynamics of Airfoils 2 C-3: Panel Methods C-4: Thin Airfoil Theory AE301 Aerodynamics I : List of Subjects
XI.C. Power-Off Stalls
References: FAA-H-8083-3; POH/AFM Objectives Key Elements Elements Schedule Equipment IP s Actions SP s Actions Completion Standards The student should develop knowledge of stalls regarding aerodynamics,
XI.B. Power-On Stalls
XI.B. Power-On Stalls References: AC 61-67; FAA-H-8083-3; POH/AFM Objectives Key Elements Elements Schedule Equipment IP s Actions SP s Actions Completion Standards The student should develop knowledge
AE2610 Introduction to Experimental Methods in Aerospace AERODYNAMIC FORCES ON A WING IN A SUBSONIC WIND TUNNEL
AE2610 Introduction to Experimental Methods in Aerospace AERODYNAMIC FORCES ON A WING IN A SUBSONIC WIND TUNNEL Objectives The primary objective of this experiment is to familiarize the student with measurement
Commentary on the Pietenpol Airfoil
Commentary on the Pietenpol Airfoil By Michael Shuck, Copyright 2004 Airfoils are really cool things. They don t exist anywhere except on paper or on computer screens or on the profile of a real, three-dimensional
DIRECCION DE PERSONAL AERONAUTICO DPTO. DE INSTRUCCION PREGUNTAS Y OPCIONES POR TEMA
MT DIREION DE PERSONL ERONUTIO DPTO. DE INSTRUION PREGUNTS Y OPIONES POR TEM 1 TEM: 0292 FLT/DSP - (HP. 03) ERODYNMIS OD_PREG: PREG20084823 (8324) PREGUNT: When are inboard ailerons normally used? Low-speed
A103 AERODYNAMIC PRINCIPLES
A103 AERODYNAMIC PRINCIPLES References: FAA-H-8083-25A, Pilot s Handbook of Aeronautical Knowledge, Chapter 3 (pgs 4-10) and Chapter 4 (pgs 1-39) OBJECTIVE: Students will understand the fundamental aerodynamic
THEORY OF WINGS AND WIND TUNNEL TESTING OF A NACA 2415 AIRFOIL. By Mehrdad Ghods
THEORY OF WINGS AND WIND TUNNEL TESTING OF A NACA 2415 AIRFOIL By Mehrdad Ghods Technical Communication for Engineers The University of British Columbia July 23, 2001 ABSTRACT Theory of Wings and Wind
Straight and Level. Basic Concepts. Figure 1
Basic Concepts Straight and Level This lesson should start with you asking the student what they did in the last lesson, what do they remember, and determining if they have remembered correctly. We must
ENGINEERing challenge workshop for science museums in the field of aeronautic engineering
ENGINEERing challenge workshop for science museums in the field of aeronautic engineering 1 Index Workshop ID card...3 Specific unit objectives...4 Resources...4 The workshop...5 Introduction...5 The main
Four forces on an airplane
Four forces on an airplane By NASA.gov on 10.12.16 Word Count 824 Level MAX TOP: An airplane pictured on June 30, 2016. Courtesy of Pexels. BOTTOM: Four forces on an airplane. Courtesy of NASA. A force
DOWNFORCE BALANCE. The Downforce Balance graph (shown at the left) illustrates which areas of the vehicle this product affects.
OVERVIEW Spanning 67 (or 61) inches over its optimized 3D airfoil shape, the APR Performance GTC-300 Adjustable Wing supplies maximum downforce in sports and touring car applications. DOWNFORCE BALANCE
LAPL(A)/PPL(A) question bank FCL.215, FCL.120 Rev PRINCIPLES OF FLIGHT 080
PRINCIPLES OF FLIGHT 080 1 Density: Is unaffected by temperature change. Increases with altitude increase. Reduces with temperature reduction. Reduces with altitude increase. 2 The air pressure that acts
THE DESIGN OF WING SECTIONS
THE DESIGN OF WING SECTIONS Published in "Radio Control Model News" Issue Number 8 Winter 93 Aerofoil section design has advanced a great deal since great pioneers like Horatio Phillips experimented with
NORMAL TAKEOFF AND CLIMB
NORMAL TAKEOFF AND CLIMB CROSSWIND TAKEOFF AND CLIMB The normal takeoff is one in which the airplane is headed directly into the wind or the wind is very light, and the takeoff surface is firm with no
2. Page 2-13, Figure 2-19, top figure; change the green label Altitude Indicator to Attitude Indicator.
FAA-H-8083-25A Pilot s Handbook of Aeronautical Knowledge Dated 2009 Errata as of January 21, 2011 1. Page 1-18, right column, 1 st paragraph, last sentence; change the uniform resource locator (URL) to
It should be noted that the symmetrical airfoil at zero lift has no pitching moment about the aerodynamic center because the upper and
NAVWEPS -81-8 and high power, the dynamic pressure in the shaded area can be much greater than the free stream and this causes considerably greater lift than at zero thrust. At high power conditions the
DIRECCION DE PERSONAL AERONAUTICO DPTO. DE INSTRUCCION PREGUNTAS Y OPCIONES POR TEMA
MT DIREION DE PERSONL ERONUTIO DPTO. DE INSTRUION PREGUNTS Y OPIONES POR TEM 1 TEM: 0114 TP - (HP. 03) ERODYNMIS OD_PREG: PREG20078023 (8358) PREGUNT: What is the safest and most efficient takeoff and
Aerodynamic Analysis of a Symmetric Aerofoil
214 IJEDR Volume 2, Issue 4 ISSN: 2321-9939 Aerodynamic Analysis of a Symmetric Aerofoil Narayan U Rathod Department of Mechanical Engineering, BMS college of Engineering, Bangalore, India Abstract - The
Preliminary Design Review (PDR) Aerodynamics #2 AAE-451 Aircraft Design
Preliminary Design Review (PDR) Aerodynamics #2 AAE-451 Aircraft Design Aircraft Geometry (highlight any significant revisions since Aerodynamics PDR #1) Airfoil section for wing, vertical and horizontal
AERODYNAMIC CHARACTERISTICS OF NACA 0012 AIRFOIL SECTION AT DIFFERENT ANGLES OF ATTACK
AERODYNAMIC CHARACTERISTICS OF NACA 0012 AIRFOIL SECTION AT DIFFERENT ANGLES OF ATTACK SUPREETH NARASIMHAMURTHY GRADUATE STUDENT 1327291 Table of Contents 1) Introduction...1 2) Methodology.3 3) Results...5
Flying High. HHJS Science Week Background Information. Forces and Flight
Flying High HHJS Science Week 2013 Background Information Forces and Flight Flight Background Information Flying is defined as controlled movement through the air. Many things can become airborne but this
Physics for Scientist and Engineers third edition Kinematics 1-D
Kinematics 1-D The position of a runner as a function of time is plotted along the x axis of a coordinate system. During a 3.00 s time interval, the runner s position changes from x1=50.0 m to x2= 30.5
Aerodynamics. A study guide on aerodynamics for the Piper Archer
Aerodynamics A study guide on aerodynamics for the Piper Archer Aerodynamics The purpose of this pilot briefing is to discuss the simple and complex aerodynamics of the Piper Archer. Please use the following
Lesson: Airspeed Control
11/20/2018 Airspeed Control Page 1 Lesson: Airspeed Control Objectives: o Knowledge o An understanding of the aerodynamics related to airspeed control o Skill o The ability to establish and maintain a
Flight Corridor. The speed-altitude band where flight sustained by aerodynamic forces is technically possible is called the flight corridor.
Flight Corridor The speed-altitude band where flight sustained by aerodynamic forces is technically possible is called the flight corridor. The subsonic Boeing 747 and supersonic Concorde have flight corridors
Preliminary design of a high-altitude kite. A flexible membrane kite section at various wind speeds
Preliminary design of a high-altitude kite A flexible membrane kite section at various wind speeds This is the third paper in a series that began with one titled A flexible membrane kite section at high
Aerodynamic Basics Larry Bogan - Jan 2002 version MECHANICS
Aerodynamic Basics Larry Bogan - Jan 2002 version MECHANICS Vectors Force, displacement, acceleration, and velocity Inertia and Velocity Inertia is a property of mass. (When there is no force on an object,
Aviation Teleclass Webinar!
Welcome to the Supercharged Science Aviation Teleclass Webinar! You can fill out this worksheet as we go along to get the most out of time together, or you can use it as a review exercise at the end of
Transportation Engineering II Dr. Rajat Rastogi Department of Civil Engineering Indian Institute of Technology - Roorkee
Transportation Engineering II Dr. Rajat Rastogi Department of Civil Engineering Indian Institute of Technology - Roorkee Lecture - 28 Aircraft Characteristics Dear students, I welcome you back to the lecture
NASA Engineering Design Challenge The Great Boomerang Challenge Teacher Guide Overview your students excited about this lesson
NASA Engineering Design Challenge The Great Boomerang Challenge Teacher Guide Overview Students think and act like engineers and scientists as they follow the eight steps of the engineering design process
See the diagrams at the end of this manual for judging position locations.
Landing Events Penalties General Judges should use airport diagrams, satellite pictures or other means to determine, as accurately as possible, assessments of landing pattern penalties. Judges should be
NAME:... SCHOOL: LINEAR MOTION. Answer ALL questions in this paper in the spaces provided.
NAME:.... SCHOOL: DATE:... LINEAR MOTION INSTRUCTIONS TO CANDIDATES Answer ALL questions in this paper in the spaces provided. 1. Two forces that act on a moving cyclist are the driving force and the resistive
Sportsman (401) Maneuver Descriptions. And. Suggested Downgrades
Sportsman (401) Maneuver Descriptions And Suggested Downgrades 2015 Purpose: The purpose of this guide is to furnish an accurate description of each maneuver of the Sportsman (401) pattern sequence. Study
Things to remember when flying N102RE or any Taildragger
Page 1 of 8 Things to remember when flying N102RE or any Taildragger 1. The Center of Gravity (CG) is behind the main between a taildragger (i.e. conventional gear airplane) and a tricycle gear airplane
PHYSICS 12 NAME: Kinematics and Projectiles Review
NAME: Kinematics and Projectiles Review (1-3) A ball is thrown into the air, following the path shown in the diagram. At 1, the ball has just left the thrower s hand. At 5, the ball is at its original
Table of Contents. Career Overview... 4
Table of Contents Career Overview.................................................. 4 Basic Lesson Plans Hot-Air Balloons Activity 1 Your First Hot-Air Balloon.... 5 Activity 2 Surface Area and Volume...
VIII.A. Straight and Level Flight
VIII.A. Straight and Level Flight References: FAA-H-8083-3; FAA-H-8083-25 Objectives Key Elements Elements Schedule Equipment IP s Actions SP s Actions Completion Standards The student should develop the
"Aircraft setup is a constant process really. Every
The R/C Aircraft Proving Grounds - Aerobatics Setup Set Up for Success by: Douglas Cronkhite "Aircraft setup is a constant process really. Every time something is changed, there is the chance it will affect
Aircraft Stability and Performance 2nd Year, Aerospace Engineering. Dr. M. Turner
Aircraft Stability and Performance 2nd Year, Aerospace Engineering Dr. M. Turner Basic Info Timetable 15.00-16.00 Monday Physics LTA 16.00-17.00 Monday Physics LTA Exam 2 1 2 hour exam 6 questions 2 from
Unit Review air aerodynamics and flight
SLEs Properties of Air o has pressure o has mass o composition of air Recipe for air Login to Learn Alberta site Click on Grade 6 Click on science Click on The Thrill of Flight Topic 2 What is Air?, Lesson
Gliding Into Innovation Challenge
Gliding Into Innovation Challenge Suggested Target Level Middle School & High School Suggested Timeline Engineering Challenge As a member of a Flight Design Team, you will produce a design that incorporates
VIII.A. Straight and Level Flight
VIII.A. Straight and Level Flight References: FAA-H-8083-3; FAA-H-8083-25 Objectives Key Elements Elements Schedule Equipment IP s Actions SP s Actions Completion Standards The student should develop the
CHAPTER 9 PROPELLERS
CHAPTER 9 CHAPTER 9 PROPELLERS CONTENTS PAGE How Lift is Generated 02 Helix Angle 04 Blade Angle of Attack and Helix Angle Changes 06 Variable Blade Angle Mechanism 08 Blade Angles 10 Blade Twist 12 PROPELLERS
Front Cover Picture Mark Rasmussen - Fotolia.com
Flight Maneuvers And Stick and Rudder Skills A complete learn to fly handbook by one of aviation s most knowledgeable and experienced flight instructors Front Cover Picture Mark Rasmussen - Fotolia.com
The Physics of Flight. Outreach Program Lesson Plan
The Physics of Flight Outreach Program Lesson Plan WAAW Foundation is non-profit organization dedicated to bringing hands-on STEM education to girls all over Africa. Our Mission: To increase the pipeline
Theory of Flight Aircraft Design and Construction. References: FTGU pages 9-14, 27
Theory of Flight 6.01 Aircraft Design and Construction References: FTGU pages 9-14, 27 Main Teaching Points Parts of an Airplane Aircraft Construction Landing Gear Standard Terminology Definition The airplane
Pressure and Density Altitude
Pressure and Density Altitude Reference Sources Pilot s Handbook of Aeronautical Knowledge o Pages 9-1 to 9-4, Aircraft Performance o Pages 9-20 to 9-21, Density Altitude Charts Study Questions 1. Where
Pre Solo Written For Schweizer 2-33 Glider. Eagles Sport Aviation Club
Pre Solo Written For Schweizer 2-33 Glider Eagles Sport Aviation Club Student Date: Instructor 1) What is the maximum gross weight for the 2-33? Empty Weight? 2) What position should the trim level be
Gleim Private Pilot Flight Maneuvers Seventh Edition, 1st Printing Updates February 2018
Page 1 of 11 Gleim Private Pilot Flight Maneuvers Seventh Edition, 1st Printing Updates February 2018 If you are tested on any content not represented in our materials or this update, please share this
Homework Exercise to prepare for Class #2.
Homework Exercise to prepare for Class #2. Answer these on notebook paper then correct or improve your answers (using another color) by referring to the answer sheet. 1. Identify the major components depicted
Aerodynamics: The Wing Is the Thing
Page B1 Chapter Two Chapter Two Aerodynamics: The Wing Is the Thing The Wing Is the Thing May the Four Forces Be With You 1. [B1/3/2] The four forces acting on an airplane in flight are A. lift, weight,
Spins and how to keep the pointy end of the airplane going forward
Spins and how to keep the pointy end of the airplane going forward 8/14/07 Evan Reed, cfievan@yahoo.com Ed Williams Outline Spins and their general characteristics Accident statistics and scenarios Some
Transportation Engineering II Dr. Rajat Rastogi Department of Civil Engineering Indian Institute of Technology - Roorkee
Transportation Engineering II Dr. Rajat Rastogi Department of Civil Engineering Indian Institute of Technology - Roorkee Lecture 31 Runway Orientation Dear students, I welcome you back to the lecture series
Volume 2, Issue 5, May- 2015, Impact Factor: Structural Analysis of Formula One Racing Car
Structural Analysis of Formula One Racing Car Triya Nanalal Vadgama 1, Mr. Arpit Patel 2, Dr. Dipali Thakkar 3, Mr. Jignesh Vala 4 Department of Aeronautical Engineering, Sardar Vallabhbhai Patel Institute
CASE STUDY FOR USE WITH SECTION B
GCE A level 135/01-B PHYSICS ASSESSMENT UNIT PH5 A.M. THURSDAY, 0 June 013 CASE STUDY FOR USE WITH SECTION B Examination copy To be given out at the start of the examination. The pre-release copy must
Aviation Teleclass Webinar!
Name Welcome to the Supercharged Science Aviation Teleclass Webinar! You can fill out this worksheet as we go along to get the most out of time together, or you can use it as a review exercise at the end
Principles of Flight. Chapter 4. From the Library at Introduction. Structure of the Atmosphere
From the Library at www.uavgroundschool.com Chapter 4 Principles of Flight Introduction This chapter examines the fundamental physical laws governing the forces acting on an aircraft in flight, and what
Exam Unit 5: Motion and Forces
Exam Unit 5: Motion and Forces 1. Aleshia is moving forward at constant speed of 2 m/s. Which statement correctly describes Aleshia s movement? A. Her speed is increasing by 2 m/s every second. B. She
LAPL/PPL question bank FCL.215, FCL.120 Rev PRINCIPLES OF FLIGHT 080
LAPL/PPL question bank FCL.215, FCL.120 Rev. 1.7 11.10.2018 PRINCIPLES OF FLIGHT 080 1 Density: Reduces with temperature reduction. Increases with altitude increase. Reduces with altitude increase. Is
NSRCA Club or Novice Class. Maneuver Descriptions. And. Suggested Downgrades
NSRCA Club or Novice Class Maneuver Descriptions And Suggested Downgrades August 18, 2016 Purpose: The purpose of this guide is to furnish an accurate description of each maneuver of the NSRCA Club or
Aviation Supplies & Academics, Inc nd Place SE Newcastle, Washington (425)
The Pilot s Manual 2: Ground School Aviation Supplies & Academics, Inc. 7005 132nd Place SE Newcastle, Washington 98059-3153 (425) 235-1500 www.asa2fly.com Originally published by Center for Aviation Theory
AIRCRAFT STRUCTURAL DESIGN & ANALYSIS K. RAMAJEYATHILAGAM
AIRCRAFT STRUCTURAL DESIGN & ANALYSIS K. RAMAJEYATHILAGAM To invent an airplane is nothing To build one is something But to fly is everything Lilienthal DAY 1 WHAT IS AN AIRCRAFT? An aircraft is a vehicle,
PERFORMANCE MANEUVERS
Ch 09.qxd 5/7/04 8:14 AM Page 9-1 PERFORMANCE MANEUVERS Performance maneuvers are used to develop a high degree of pilot skill. They aid the pilot in analyzing the forces acting on the airplane and in
Aircraft - Very Heavy Lift at Very Low Cost
Aircraft - Very Heavy Lift at Very Low Cost Stephen Funck This is a span loader for standard shipping containers. The design goal is the lowest cost per ton / mile. Low wing loading allows for low flight
NAME:... SCHOOL: FORCE INSTRUCTIONS TO CANDIDATES. Answer ALL questions in this paper in the spaces provided.
NAME:.... SCHOOL: DATE:... FORCE INSTRUCTIONS TO CANDIDATES Answer ALL questions in this paper in the spaces provided. 1. Sally pulls a sledge in the snow. friction F (a) (i) Draw an arrow on the rope
Lesson: Pitch Trim. Materials / Equipment Publications o Flight Training Manual for Gliders (Holtz) Lesson 4.4 Using the Trim Control.
11/18/2015 Pitch Trim Page 1 Lesson: Pitch Trim Objectives: o Knowledge o An understanding of the aerodynamics related to longitudinal (pitch) stability o Skill o Use of the pitch trim system to control
INTRODUCTION TO FLIGHT (REVIEW, AEROSPACE DIMENSIONS, MODULE 1)
INTRODUCTION TO FLIGHT (REVIEW, AEROSPACE DIMENSIONS, MODULE 1) CAPTAIN. JERRY PAINTER AEROSPACE EDUCATION OFFICER COMPOSITE SQUADRON 316, (CIVIL AIR PATROL) CASA GRANDE, ARIZONA IMPORTANT TERMS-THE LANGUAGE