Uncontrolled copy not subject to amendment. Principles of Flight

Size: px
Start display at page:

Download "Uncontrolled copy not subject to amendment. Principles of Flight"

Transcription

1 Uncontrolled copy not subject to amendment Principles of Flight

2 Principles of Flight Learning Outcome 2: Understand how the stability of an aeroplane is maintained in flight and how manoeuvrability is controlled Part 1

3 Principles of Flight H Copter B Loons A Ship A Bourne R Way C Tower S Huttle Dan Winterland I Flyum Revision

4 Questions What is the force called that drives an aircraft forwards? Lift Weight Drag Thrust

5 Questions What is the force called that resists the forward motion of an aircraft? Lift Weight Drag Thrust

6 Questions If your speed is doubled, by how much would the Drag be increased? x2 x4 x6 x8

7 Questions If Thrust = Drag and Lift = Weight then the aircraft is: Climbing Flying Straight & Level and Accelerating Flying Straight & Level an Decelerating Flying Straight & Level at Constant Speed

8 Stability Objectives: 1. Identify the Axes of Rotation for an Aircraft. 2. Identify the Planes of Movement for an Aircraft. 3. Describe and Explain Stability in the 3 Planes of Movement. 4. Explain Dihedral and Anhedral and how they affect Stability.

9 OW!! Stability What would happen to this dart when thrown? What would happen now? Something is needed to Stabilise the Dart (Aircraft).

10 Stability Airflow Centre of Gravity (CG) Airflow Body Ahead of CG is Destabilising. Body Behind CG is Stabilising.

11 Basic Stability Stable Unstable

12 Basic Stability Stable Forms of stability Static - initial reaction Dynamic - subsequent reaction

13 Basic Stability Stable Forms of stability Static - initial reaction Dynamic - subsequent reaction

14 Basic Stability Stable Forms of stability Static - initial reaction Dynamic - subsequent reaction

15 Basic Stability Stable Forms of stability Static - initial reaction Dynamic - subsequent reaction

16 Basic Stability Stable Forms of stability Static - initial reaction Dynamic - subsequent reaction

17 Application to Aircraft Static Stability Unstable Neutral Stable

18 Application to Aircraft Statically Stable Dynamic Stability Dynamically Neutral Dynamically Unstable Dynamically Stable

19 Planes of Stabilisation Pitch (Longitudinal) Yaw (Directional) Longitudinal Axis Roll (Lateral) Lateral Axis Normal Axis

20 Stabilisation Axis Plane Stability Longitudinal Rolling Lateral

21 Stability

22 Stabilisation Axis Plane Stability Longitudinal Rolling Lateral Lateral Pitching Longitudinal

23 Stability

24 Stabilisation Axis Plane Stability Longitudinal Rolling Lateral Lateral Pitching Longitudinal Normal Yawing Directional

25 Stability

26

27 Directional Stability

28 Directional Stability Flight Path CG Lift Stabilising Influence of fin: 1. Value of Lift 2. Moment Arm Enhancement features: A large fin Something and/or a long causes moment the aircraft arm to yaw

29 CofG Considerations

30 The strange case of the ever growing fins

31

32 Longitudinal Stability

33 Longitudinal Stability Lift Flight Path Weight

34 Longitudinal Stability Lift Lift Flight Path Weight

35 Lateral Stability

36 Lateral Stability Lift Resultant Sideslip

37 Lateral Stability Hdg Aircraft sideslips in this direction

38 Lateral Stability Methods Large Fin of high aspect ratio (a big tall fin). Lift from fin rolls wings level

39 Lateral Stability Methods hedral: Due to new direction of relative airflow r wing has higher AoA than upper - more lift - tends ll wings level. Lift

40 Lateral Stability Methods 3. Sweepback Span Chord Aspect Ratio More Less Higher Less More Lower Lift More Less LOW WING

41 Lateral Stability Methods 4. High wing Less Lift More Lift low near wing roots affected selage - Increases AoA on

42 Lateral Stability Methods 1. High Fin. 2. Dihedral. 3. Sweepback. 4. High Mounted Wing ut too much Lateral Stability High wing and Sweepback) ery undesirable in fighter aircraft. Therefore anhedral to reduce the excess

43 Any Questions?

44 Stability jectives: Identify the Axes of Rotation for an Aircraft. Identify the Planes of Movement for an Aircraft. Describe and Explain Stability in the 3 Planes of Movement. Explain Dihedral and Anhedral and how they affect Stability.

45 Questions at are the 3 planes of an aircraft s movement? Pitching, Lateral and Rolling. Pitching, Rolling and Yawing. Yawing, Longitudinal and Rolling.

46 Questions ich one of the following will REDUCE Lateral Stability? edral. arge Fin. eepback.

47 Questions at are the 3 Axes about which an Aircraft can move? Pitching, Lateral and Longitudinal. Pitching, Rolling and Yawing. Yawing, Longitudinal and Normal.

48 Questions ich 3 Terms describe Static Stability? Stable, Neutral and Unstable. Stable, Rolling and Unstable. Yawing, Neutral and Stable.

49

Stability and Flight Controls

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

More information

Principles of glider flight

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 &

More information

Aerodynamics Principles

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

More information

Uncontrolled copy not subject to amendment. Principles of Flight

Uncontrolled copy not subject to amendment. Principles of Flight Uncontrolled copy not subject to amendment Principles of Flight Principles of Flight Learning Outcome 1: Know the principles of lift, weight, thrust and drag and how a balance of forces affects an aeroplane

More information

LAPL(A)/PPL(A) question bank FCL.215, FCL.120 Rev PRINCIPLES OF FLIGHT 080

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

More information

PEMP ACD2501. M.S. Ramaiah School of Advanced Studies, Bengaluru

PEMP ACD2501. M.S. Ramaiah School of Advanced Studies, Bengaluru Aircraft Performance, Stability and Control Session delivered by: Mr. Ramjan Pathan 1 Session Objectives Aircraft Performance: Basicsof performance (t (steadystateand tt d accelerated) Performance characteristics

More information

Preliminary Design Review (PDR) Aerodynamics #2 AAE-451 Aircraft Design

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

More information

wind wobble unstable

wind wobble unstable Rocket Stability During the flight of a model rocket, gusts of wind or thrust instabilities, can cause the rocket to "wobble", or change its attitude in flight. Poorly built or designed rockets can also

More information

LAPL/PPL question bank FCL.215, FCL.120 Rev PRINCIPLES OF FLIGHT 080

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

More information

Aerodynamics. A study guide on aerodynamics for the Piper Archer

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

More information

V mca (and the conditions that affect it)

V mca (and the conditions that affect it) V mca (and the conditions that affect it) V mca, the minimum airspeed at which an airborne multiengine airplane is controllable with an inoperative engine under a standard set of conditions, is arguably

More information

Winnipeg Headingley Aero Modellers. Things About Airplanes.

Winnipeg Headingley Aero Modellers. Things About Airplanes. Winnipeg Headingley Aero Modellers Things About Airplanes. Table of Contents Introduction...2 The Airplane...2 How the Airplane is Controlled...3 How the Airplane Flies...6 Lift...6 Weight...8 Thrust...9

More information

Learning Objectives 081 Principles of Flight

Learning Objectives 081 Principles of Flight Learning Objectives 081 Principles of Flight Conventions for questions in subject 081. 1. The following standard conventions are used for certain mathematical symbols: * multiplication. > = greater than

More information

XI.B. Power-On Stalls

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

More information

XI.C. Power-Off Stalls

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,

More information

II.E. Airplane Flight Controls

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

More information

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 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

More information

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. 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

More information

No Description Direction Source 1. Thrust

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

More information

DIRECCION DE PERSONAL AERONAUTICO DPTO. DE INSTRUCCION PREGUNTAS Y OPCIONES POR TEMA

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

More information

A103 AERODYNAMIC PRINCIPLES

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

More information

Chapter 3: Aircraft Construction

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,

More information

THE AIRCRAFT IN FLIGHT Issue /07/12

THE AIRCRAFT IN FLIGHT Issue /07/12 1 INTRODUCTION This series of tutorials for the CIX VFR Club are based on real world training. Each document focuses on a small part only of the necessary skills required to fly a light aircraft, and by

More information

Detailed study 3.4 Topic Test Investigations: Flight

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

More information

II.D. Principles of Flight

II.D. Principles of Flight II.D. Principles of 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 knowledge

More information

JAA Administrative & Guidance Material Section Five: Licensing, Part Two: Procedures

JAA Administrative & Guidance Material Section Five: Licensing, Part Two: Procedures INTRODUCTION Conventions for questions in subject 081. 1. The following standard conventions are used for certain mathematical symbols: * multiplication. >= greater than or equal to.

More information

CHAPTER 9 PROPELLERS

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

More information

Four forces on an airplane

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

More information

PRINCIPLES OF FLIGHT

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

More information

CHAPTER 1 - PRINCIPLES OF FLIGHT

CHAPTER 1 - PRINCIPLES OF FLIGHT CHAPTER 1 - PRINCIPLES OF FLIGHT Reilly Burke 2005 INTRODUCTION There are certain laws of nature or physics that apply to any object that is lifted from the Earth and moved through the air. To analyze

More information

DEFINITIONS. Aerofoil

DEFINITIONS. Aerofoil Aerofoil DEFINITIONS An aerofoil is a device designed to produce more lift (or thrust) than drag when air flows over it. Angle of Attack This is the angle between the chord line of the aerofoil and the

More information

PRE-TEST Module 2 The Principles of Flight Units /60 points

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

More information

ATPL Principles of Flight - deel 2

ATPL Principles of Flight - deel 2 ATPL Principles of Flight - deel 2 1. If flaps are deployed at constant IAS in straight and level flight, the magnitude of tip vortices will eventually: (flap span less then wing span) A decrease B remain

More information

Aircraft Stability and Performance 2nd Year, Aerospace Engineering. Dr. M. Turner

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

More information

DIRECCION DE PERSONAL AERONAUTICO DPTO. DE INSTRUCCION PREGUNTAS Y OPCIONES POR TEMA

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

More information

WHAT IS GLIDER? A light engineless aircraft designed to glide after being towed aloft or launched from a catapult.

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

More information

Aero Club. Introduction to Flight

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

More information

PERFORMANCE VS INTERCEPTOR EXTENSION

PERFORMANCE VS INTERCEPTOR EXTENSION PERFORMANCE VS INTERCEPTOR EXTENSION Misleading information is circulating that claims interceptors with a large stroke and small span are better than Zipwake s wide span interceptors with a smaller stroke.

More information

Flight Control Systems Introduction

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

More information

PILOT S HANDBOOK of Aeronautical Knowledge AC61-23C

PILOT S HANDBOOK of Aeronautical Knowledge AC61-23C PILOT S HANDBOOK of Aeronautical Knowledge AC61-23C Revised 1997 Chapter 1 Excerpt Compliments of... www.alphatrainer.com Toll Free: (877) 542-1112 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION

More information

Ottawa Remote Control Club Wings Program

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

More information

Aircraft Stability and Control Prof. A. K. Ghosh Department of Aerospace Engineering Indian Institute of Technology-Kanpur. Lecture- 25 Revision

Aircraft Stability and Control Prof. A. K. Ghosh Department of Aerospace Engineering Indian Institute of Technology-Kanpur. Lecture- 25 Revision Aircraft Stability and Control Prof. A. K. Ghosh Department of Aerospace Engineering Indian Institute of Technology-Kanpur Lecture- 25 Revision Yes, dear friends, this is the mann ki baat session for lateral

More information

The Fly Higher Tutorial IV

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

More information

Analysis of the Z-wing configuration

Analysis of the Z-wing configuration School of Innovation, Design and Engineering BACHELOR THESIS IN AERONAUTICAL ENGINEERING 15 CREDITS, BASIC LEVEL 300 Analysis of the Z-wing configuration Author: Joakim Avén Report code: MDH.IDT.FLYG.0231.2011.GN300.15HP.Ae

More information

Designing a Model Rocket

Designing a Model Rocket Designing a Model Rocket Design Components In the following pages we are going to look at the design requirements for a stable single stage model rocket. From the diagram here you can see that the rocket

More information

PRINCIPLES OF FLIGHT

PRINCIPLES OF FLIGHT PRINCIPLES OF FLIGHT A BASIC OVERVIEW Bruce Wall 1982 _ DEFINITIONS AEROFOIL This term is used to describe the curved cross AXES OF MOVEMENT sectional design of an aeroplane wing. Normally, the cross sectional

More information

POWERED FLIGHT HOVERING FLIGHT

POWERED FLIGHT HOVERING FLIGHT Once a helicopter leaves the ground, it is acted upon by the four aerodynamic forces. In this chapter, we will examine these forces as they relate to flight maneuvers. POWERED FLIGHT In powered flight

More information

Stability & Control Aspects of UCAV Configurations

Stability & Control Aspects of UCAV Configurations Stability & Control Aspects of UCAV Configurations Paul Flux Senior Aerodynamicist BAE SYSTEMS Air Programmes Report Documentation Page Form Approved OMB No. 0704-0188 Public reporting burden for the collection

More information

C-130 Reduction in Directional Stability at Low Dynamic Pressure and High Power Settings

C-130 Reduction in Directional Stability at Low Dynamic Pressure and High Power Settings C-130 Reduction in Directional Stability at Low Dynamic Pressure and High Power Settings The C-130 experiences a marked reduction of directional stability at low dynamic pressures, high power settings,

More information

The Metric Glider. By Steven A. Bachmeyer. Aerospace Technology Education Series

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

More information

It should be noted that the symmetrical airfoil at zero lift has no pitching moment about the aerodynamic center because the upper and

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

More information

Flying Wings. By Henry Cole

Flying Wings. By Henry Cole Flying Wings By Henry Cole FLYING WINGS REPRESENT THE THEORETICAL ULTIMATE IN AIRCRAFT DESIGN. USE THESE IDEAS, AVAILABLE AFTER A YEAR, OF RESEARCH, TO DEVELOP PRACTICAL MODELS. The rubber version of this

More information

A-CR-CCP-803/PF-001 CHAPTER 12 PO 331 DESCRIBE PRINCIPLES OF FLIGHT

A-CR-CCP-803/PF-001 CHAPTER 12 PO 331 DESCRIBE PRINCIPLES OF FLIGHT CHAPTER 12 PO 331 DESCRIBE PRINCIPLES OF FLIGHT ROYAL CANADIAN AIR CADETS PROFICIENCY LEVEL THREE INSTRUCTIONAL GUIDE SECTION 1 EO M331.01 DESCRIBE AIRCRAFT STABILITY Total Time: 60 min PREPARATION PRE-LESSON

More information

Table of Contents. Career Overview... 4

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...

More information

RESEARCH MEMORANDUM. WASHINGTON December 3, AERODYNl$MIC CHARACTERISTICS OF A MODEL? OF AN ESCAPE ...,

RESEARCH MEMORANDUM. WASHINGTON December 3, AERODYNl$MIC CHARACTERISTICS OF A MODEL? OF AN ESCAPE ..., .". -.%. ;& RESEARCH MEMORANDUM AERODYNl$MIC CHARACTERISTICS OF A MODEL? OF AN ESCAPE 1 \ < :. By John G. Presnell, Jr. w'..., '.., 3... This material contains information affecting the National Bfense

More information

Uncontrolled copy not subject to amendment. Principles of Flight

Uncontrolled copy not subject to amendment. Principles of Flight Uncontrolled copy not subject to amendment Principles of Flight Principles of Flight Learning Outcome 3: Know the principles of stalling Principles of Flight Revision Questions What effect does a Trailing

More information

Part 66 Cat. B1 / B2 Module 8 BASIC AERODYNAMICS. Vilnius Issue 1. Effective date FOR TRAINING PURPOSES ONLY Page 1 of 74

Part 66 Cat. B1 / B2 Module 8 BASIC AERODYNAMICS. Vilnius Issue 1. Effective date FOR TRAINING PURPOSES ONLY Page 1 of 74 Part 66 Cat. B1 / B2 Module 8 BASIC AERODYNAMICS Vilnius-2017 Issue 1. Effective date 2017-07-28 FOR TRAINING PURPOSES ONLY Page 1 of 74 Table of Contents Part-66 Module 8. Basic Aerodynamics (Cat. B1

More information

OUTLINE SHEET BASIC THEORY. 2.1 DEFINE scalar, in a classroom, in accordance with Naval Aviation Fundamentals, NAVAVSCOLSCOM-SG-200

OUTLINE SHEET BASIC THEORY. 2.1 DEFINE scalar, in a classroom, in accordance with Naval Aviation Fundamentals, NAVAVSCOLSCOM-SG-200 Sheet 1 of 7 OUTLINE SHEET 2-1-1 BASIC THEORY A. INTRODUCTION This lesson is a basic introduction to the theory of aerodynamics. It provides a knowledge base in aerodynamic mathematics, air properties,

More information

air cadet publication

air cadet publication air cadet publication ACP 33 flight volume 2 - principles of flight No Amendment List Date Amended by Date Incorporated 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 i ACP 33 FLIGHT CONTENTS Volume 1... History

More information

Straight and Level. Basic Concepts. Figure 1

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

More information

Flightlab Ground School 7. Longitudinal Dynamic Stability

Flightlab Ground School 7. Longitudinal Dynamic Stability Flightlab Ground School 7. Longitudinal Dynamic Copyright Flight Emergency & Advanced Maneuvers Training, Inc. dba Flightlab, 2009. All rights reserved. For Training Purposes Only Introduction to is the

More information

Aircraft Stability and Control Prof. A.K.Ghosh Department of Aerospace Engineering Indian Institute of Technology-Kanpur. Lecture-01 Introduction

Aircraft Stability and Control Prof. A.K.Ghosh Department of Aerospace Engineering Indian Institute of Technology-Kanpur. Lecture-01 Introduction Aircraft Stability and Control Prof. A.K.Ghosh Department of Aerospace Engineering Indian Institute of Technology-Kanpur Lecture-01 Introduction Wish you all very, very happy New Year. We are on the tarmac

More information

AE Stability and Control of Aerospace Vehicles

AE Stability and Control of Aerospace Vehicles AE 430 - Stability and Control of Aerospace Vehicles Introduction 1 Welcome to AE 430 - Stability and Control of Aerospace Vehicles Pier Marzocca Pier CAMP 234, MAE Department MW 10:00-12:30, CAMP 234

More information

LEVEL FOUR AVIATION EVALUATION PRACTICE TEST

LEVEL FOUR AVIATION EVALUATION PRACTICE TEST Below you will find a practice test for the Level 4 Aviation Evaluation that covers PO431, PO432, PO436, and PO437. It is recommended that you focus on the material covered in the practice test as you

More information

Flying High. HHJS Science Week Background Information. Forces and Flight

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

More information

FUSELAGE-MOUNTED FINS ON THE STATIC DIRECTIONAL STABILITY. By M. Leroy Spearman, Ross B. Robinson, and Cornelius Driver

FUSELAGE-MOUNTED FINS ON THE STATIC DIRECTIONAL STABILITY. By M. Leroy Spearman, Ross B. Robinson, and Cornelius Driver RESEARCH MEMORANDUM THE EFFECTS OF THE ADDITION OF SMALL FUSELAGE-MOUNTED FINS ON THE STATIC DIRECTIONAL STABILITY CHARACTERISTICS OF A MODEL OF A 45' SWEPT-WING AIRPLANE AT ANGLES OF ATTACK UP TO 15.3?

More information

The Tingalpa March April 2008 TRANSMITTER. 40 years at Porter s Field Tingalpa Model Aero Club

The Tingalpa March April 2008 TRANSMITTER. 40 years at Porter s Field Tingalpa Model Aero Club The Tingalpa March April 2008 TRANSMITTER 40 years at Porter s Field 1968 2008 Tingalpa Model Aero Club WWW.tmac.asn.au MANAGEMENT COMMITTEE President. Peter Stevenson 0401 700 675 President@tmac.asn.au

More information

Credit value: 10 Guided learning hours: 60

Credit value: 10 Guided learning hours: 60 Unit 66: Theory of Flight Unit code: QCF Level 3: Credit value: 10 Guided learning hours: 60 Aim and purpose A/600/7123 BTEC Nationals This unit will provide learners with an understanding of the atmosphere

More information

Aerobatic Trimming Chart

Aerobatic Trimming Chart Aerobatic Trimming Chart From RCU - Chip Hyde addresses his view of Engine/Motor thrust. I run almost no right thrust in my planes and use the thottle to rudd mix at 2% left rudd. to throttle at idle.

More information

Aviation Merit Badge Knowledge Check

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

More information

Theory of Flight Aircraft Design and Construction. References: FTGU pages 9-14, 27

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

More information

Theory of Flight Stalls. References: FTGU pages 18, 35-38

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

More information

VIII.A. Straight and Level Flight

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

More information

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. 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

More information

The Principles of Flight for Pilots P. J. Swatton

The Principles of Flight for Pilots P. J. Swatton The Principles of Flight for Pilots P. J. Swatton A John Wiley and Sons, Ltd., Publication The Principles of Flight for Pilots Aerospace Series List Cooperative Path Planning of Unmanned Aerial Tsourdos

More information

CASE STUDY FOR USE WITH SECTION B

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

More information

Advanced Stalling. L = CL ½ ρ V 2 S. L = angle of attack x airspeed. h L = angle of attack x h airspeed. Advanced Manoeuvres

Advanced Stalling. L = CL ½ ρ V 2 S. L = angle of attack x airspeed. h L = angle of attack x h airspeed. Advanced Manoeuvres Advanced Manoeuvres Advanced Stalling This Advanced Stalling lesson covers the factors that affect the observed airspeed and nose attitude at the stall. Although the aeroplane always stalls when the aerofoil

More information

Give Wings to Imagination

Give Wings to Imagination Give Wings to Imagination Water rocket uses water as a propellant. PRINCIPLE It is based on the NEWTON S THIRD LAW OF MOTION. For a simple model, water rocket consists of a bottle having water above

More information

Homework Exercise to prepare for Class #2.

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

More information

AIRCRAFT PRIMARY CONTROLS A I R C R A F T G E N E R A L K N O W L E D G E

AIRCRAFT PRIMARY CONTROLS A I R C R A F T G E N E R A L K N O W L E D G E 1.02.02 AIRCRAFT PRIMARY CONTROLS 1. 0 2 A I R C R A F T G E N E R A L K N O W L E D G E CONTROLLING AIRCRAFT AIRCRAFT CONTROL SYSTEM In general, we use control inputs of the following devices in cabin:

More information

Exploration Series. AIRPLANE Interactive Physics Simulation Page 01

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,

More information

Related Careers: Aircraft Instrument Repairer Aircraft Designer Aircraft Engineer Aircraft Electronics Specialist Aircraft Mechanic Pilot US Military

Related Careers: Aircraft Instrument Repairer Aircraft Designer Aircraft Engineer Aircraft Electronics Specialist Aircraft Mechanic Pilot US Military Airplane Design and Flight Fascination with Flight Objective: 1. You will be able to define the basic terms related to airplane flight. 2. You will test fly your airplane and make adjustments to improve

More information

INTRODUCTION TO FLIGHT (REVIEW, AEROSPACE DIMENSIONS, MODULE 1)

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

More information

Principles of glider flight

Principles of glider flight Principles of glider flight [ Lecture 1: Lift, drag & glide performance ] Richard Lancaster Email: Richard@RJPLancaster.net Twitter: @RJPLancaster ASK-21 illustrations Copyright 1983 Alexander Schleicher

More information

Aerodynamics of Flight

Aerodynamics of Flight Chapter 4 Aerodynamics of Flight Forces Acting on the Aircraft Thrust, drag, lift, and weight are forces that act upon all aircraft in flight. Understanding how these forces work and knowing how to control

More information

MANOEUVRING BOOKLET V1.06

MANOEUVRING BOOKLET V1.06 MANOEUVRING BOOKLET V.6 Mathematical model of VLCC (Dis.769t) bl. Version: v Dll Version:.3.558 According : Solas II-, regulation 8.3 St. Petersburg 6 . GENERAL DESCRIPTION.. Ships particulars... Ships

More information

Front Cover Picture Mark Rasmussen - Fotolia.com

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

More information

A COMPUTATIONAL STUDY ON THE DESIGN OF AIRFOILS FOR A FIXED WING MAV AND THE AERODYNAMIC CHARACTERISTIC OF THE VEHICLE

A COMPUTATIONAL STUDY ON THE DESIGN OF AIRFOILS FOR A FIXED WING MAV AND THE AERODYNAMIC CHARACTERISTIC OF THE VEHICLE 28 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES A COMPUTATIONAL STUDY ON THE DESIGN OF AIRFOILS FOR A FIXED WING MAV AND THE AERODYNAMIC CHARACTERISTIC OF THE VEHICLE Jung-Hyun Kim*, Kyu-Hong

More information

PRIMARY FLIGHT CONTROLS. AILERONS Ailerons control roll about the longitudinal axis. The ailerons are attached to the outboard trailing edge of

PRIMARY FLIGHT CONTROLS. AILERONS Ailerons control roll about the longitudinal axis. The ailerons are attached to the outboard trailing edge of Aircraft flight control systems are classified as primary and secondary. The primary control systems consist of those that are required to safely control an airplane during flight. These include the ailerons,

More information

AERODYNAMICS VECTORS

AERODYNAMICS VECTORS AERODYNAMICS The challenge in explaining aerodynamics for glider pilots is to provide the information needed to fly safely and efficiently without overloading the student with complex theories. Meeting

More information

MANOEUVRING BOOKLET V1.06

MANOEUVRING BOOKLET V1.06 MANOEUVRING BOOKLET V1.6 Mathematical model of Integrated Tug Barge 45 Version: v9 Dll Version: 2.31.558 According to: Solas II-1, regulation 28.3 St. Petersburg 26 1. GENERAL DESCRIPTION 1.1. Ships particulars

More information

11-1. Horizontal tailplane sizing according to control requirement

11-1. Horizontal tailplane sizing according to control requirement 11-1 11 Empennage izing In ection Empennage General Design, the areas of the horizontal and vertical tailplanes were calculated merely with the aid of tail volume coefficients. The tail lever arms were

More information

HOW AND WHY DO GLIDERS FLY - WHAT SHAPE SHOULD THEY BE?

HOW AND WHY DO GLIDERS FLY - WHAT SHAPE SHOULD THEY BE? HOW AND WHY DO GLIDERS FLY - WHAT SHAPE SHOULD THEY BE? What is flight? We all understand that air is a fluid, not dissimilar to, if lighter than, water, and we can all appreciate that an immerse body

More information

FORCES ACTING ON THE AIRPLANE

FORCES ACTING ON THE AIRPLANE CH 03.qxd 10/24/03 6:44 AM Page 3-1 FORCES ACTING ON THE AIRPLANE In some respects at least, how well a pilot performs in flight depends upon the ability to plan and coordinate the use of the power and

More information

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 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

More information

Fighter aircraft design. Aerospace Design Project G. Dimitriadis

Fighter aircraft design. Aerospace Design Project G. Dimitriadis Fighter aircraft design Aerospace Design Project 2017-2018 G. Dimitriadis General configuration The elements of the general configuration are the following: Wing Wing placement Airfoil Number of engines

More information

Lesson: Airspeed Control

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

More information

Stalls and Spins. Tom Johnson CFIG

Stalls and Spins. Tom Johnson CFIG Stalls and Spins Tom Johnson CFIG Contents Angle of Attack Stall Recognition and Recovery Spin Entry and Recovery Load Limit Considerations Gust Induced Stall and Spin Accidents Stalls a stall is a loss

More information

Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, Figures

Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, Figures Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 5 Wing Design Figures 1 Identify and prioritize wing design requirements (Performance, stability, producibility, operational

More information

CIRCLING THE HOLIGHAUS WAY -

CIRCLING THE HOLIGHAUS WAY - CIRCLING THE HOLIGHAUS WAY - OR DO YOU REALLY WANT TO KEEP THE YAW STRING CENTERED? BY RICHARD H. JOHNSON ANSWERS: 1. During Straight Flight - YES, that minimizes drag and maximizes the sailplane's performance.

More information