Theory of Flight. Main Teaching Points. Definition Parts of an Airplane Aircraft Construction Landing Gear Standard Terminology

Similar documents
Chapter 3: Aircraft Construction

Aircraft Maintenance Prof. A.K Ghosh Prof. Vipul Mathur Department of Aerospace Engineering Indian Institute of Technology, Kanpur

SD3-60 AIRCRAFT MAINTENANCE MANUAL. This chapter includes information on dimensions, areas, zoning, etc. and is presented as follows:

Preliminary Detailed Design Review

MD RA Minister's Delegates - Recreational Aviation Représentants du Ministre - Aviation de loisir

The Airplane That Could!

MD - RA. Minister s Delegates - Recreational Aviation Représentants du Ministre - Aviation de Loisir Service d Inspection

CHAPTER 10. WEIGHT AND BALANCE

CONCEPTUAL DESIGN OF ECOLOGICAL AIRCRAFT FOR COMMUTER AIR TRANSPORTATION

FUNDAMENTALS OF ROTOR AND POWER TRAIN MAINTENANCE TECHNIQUES AND PROCEDURES

AIRCRAFT DESIGN SUBSONIC JET TRANSPORT

PAC 750XL PAC 750XL PAC-750XL

Aircraft Design Conceptual Design

AERONAUTICAL ENGINEERING

State of Israel Ministry of Transport Civil Aviation Authority TYPE CERTIFICATE DATA SHEET

AE 451 Aeronautical Engineering Design Final Examination. Instructor: Prof. Dr. Serkan ÖZGEN Date:

Design, Build, Fly Q&A #1

Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 3 Aircraft Conceptual Design. Tables

Ultralight airplane Design

Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 11 Aircraft Weight Distribution Tables

Prop effects (Why we need right thrust) Torque reaction Spiraling Slipstream Asymmetric Loading of the Propeller (P-Factor) Gyroscopic Precession

Amendment List. Crown Copyright 2007

SIMULATION OF PROPELLER EFFECT IN WIND TUNNEL

New Design Concept of Compound Helicopter

DUCHESS BE-76 AND COMMERCIAL MULTI ADD-ON ORAL REVIEW FOR CHECKRIDE

SAE Aero Design. Mid-point Review 3/10/2016. By Ali Alqalaf, Jasem Alshammari, Dong Yang Cao, Darren Frankenberger, Steven Goettl, and John Santoro

Design Considerations for Stability: Civil Aircraft

AE 440: Conceptual Design Report for the Agricultural Unmanned Aircraft System. X Duster: XD 44X

A SOLAR POWERED UAV. 1 Introduction. 2 Requirements specification

Flugzeugentwurf / Aircraft Design SS Part 35 points, 70 minutes, closed books. Prof. Dr.-Ing. Dieter Scholz, MSME. Date:

AIRCRAFT DESIGN MADE EASY. Basic Choices and Weights. By Chris Heintz

Systems Group (Summer 2012) 4 th Year (B.Eng) Aerospace Engineering Candidate Carleton University, Ottawa,Canada Mail:

2014 SAE AERO DESIGN EAST COMPETITION 10% Report

Building A Replica Aircraft. Part Three Construction Details Wings and Covering

INVESTIGATION OF ICING EFFECTS ON AERODYNAMIC CHARACTERISTICS OF AIRCRAFT AT TSAGI

FUSELAGE ASSEMBLY SECOND SECTION (of three)

THE SAGRES PROJECT - A NEW VERY LIGHT AEROPLANE. Department of Aerospace Sciences Universidade da Beira Interior Covilhã, Portugal

Powertrain Design for Hand- Launchable Long Endurance Unmanned Aerial Vehicles

European Aviation Safety Agency

CONCEPTUAL DESIGN REPORT

European Aviation Safety Agency

Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, Chapter 9 Landing Gear Design. Figures

1.1 REMOTELY PILOTED AIRCRAFTS

European Aviation Safety Agency

This manual covers all color schemes Although it only shows one color scheme, the aircraft are the same This manual is for reference to the actual

Flying Wing. Matt Statzer Bryan Williams Mike Zauberman. 17 March

2iJ AIRO2AFT CIRCTJLARS. THE GLOSTER "GAMBET t AIRPLANE. A Deck-Lding Ship's Fighter. Fitted with a 420 HP. Bristol Jupiter VI Engine

Airframes Instructor Training Manual. Chapter 6 UNDERCARRIAGE

AMT 111 Aircraft Landing Gear Systems. Chapter 13

SAE Aero Design. Apr 29, 2016

Mooney Mite M-18X Plans and Drawings Index Arranged by Group Miscellaneous Group

4.1 General Information. 4.2 Turning Radii. 4.3 Clearance Radii. 4.4 Visibility From Cockpit in Static Position. 4.5 Runway and Taxiway Turn Paths

L 298/70 Official Journal of the European Union

Aeroplane Aerodynamics and Flight Controls 1 2

SD3-60 STRUCTURAL REPAIR MANUAL

General Dynamics F-16 Fighting Falcon

European Aviation Safety Agency

AVRO LANCASTER by Ivan Pettigrew Construction Notes

Chapter No matter how you paint it, it s still going to roll, pitch and yaw. Identify Name Describe Identify Explain Describe Identify Describe

AE 451 Aeronautical Engineering Design I Estimation of Critical Performance Parameters. Prof. Dr. Serkan Özgen Dept. Aerospace Engineering Fall 2015

Agricultural Unmanned Aircraft System (AUAS)

Multidisciplinary Design Optimization of a Truss-Braced Wing Aircraft with Tip-Mounted Engines

2.2 Schedule

Aircraft Characteristics/ Aircraft Recognition

DESIGN OF A FIFTH GENERATION AIR SUPERIORITY FIGHTER AIRCRAFT

Uncontrolled copy not subject to amendment. Airframes. Revision 1.00

JODEL D.112 INFORMATION MANUAL C-FVOF

12.1 Theory of Flight Rotary Wing Aerodynamics 1 2

Irkut Corporation plant is manufacturing fuselage sections and carries out its assembly

AE 451 Aeronautical Engineering Design I Propulsion and Fuel System Integration. Prof. Dr. Serkan Özgen Dept. Aerospace Engineering December 2017

A Game of Two: Airbus vs Boeing. The Big Guys. by Valerio Viti. Valerio Viti, AOE4984, Project #1, March 22nd, 2001

Thank you again, Jim McCormick. Jabiru Pacific LLC

Towards the Optimisation of. Adaptive Aeroelastic Structures

Section 2: Basic Aerobatics

Humming Aerospace Version 9 Blade ti

AIRCRAFT CIRCULARS TATIOTAL ADVISORY COMMITTEE FOR AERONAUTICS. No A One-Place Cantilever Low-Wing Monoplane

DESIGN OF AN ARMAMENT WING FOR A LIGHT CATEGORY HELICOPTER

Instruction Manual EXTRA 260-EP. 1075mm (42.32 in) 1000mm (39.37 in) 1100gr gr. 4 channel - 4 mini servo. Axi motor 2820

SAE BRAZIL AERODESIGN COMPETITION Final Report

SAE Aero East 2017 Mid-Term Report

Chapter 9 Landing Gear Design Mohammad Sadraey Daniel Webster College

Design of Ultralight Aircraft

ECO-CARGO AIRCRAFT. ISSN: International Journal of Science, Engineering and Technology Research (IJSETR) Volume 1, Issue 2, August 2012

United States Patent (19) Cronk et al.

Chapter 10 Miscellaneous topics - 2 Lecture 39 Topics

2000/2001 AIAA Foundation Cessna/ONR Student Design Build Fly Competition. Design Report Proposal Phase

Analyzing Numerical Data: Using Ratios I.B Student Activity Sheet 5: Changing Tires

European Aviation Safety Agency

Strix Goblin Instruction Manual. Rev

Chapter 2 Lecture 5 Data collection and preliminary three-view drawing - 2 Topic

Retro. An artist rendering inspired this great 40-size sport model BY BOB NOLL AND KEN MARONI 16 MODEL AVIATION

LAA TYPE ACCEPTANCE DATA SHEET TADS 193 RANS S4 AND RANS S5 (B WING AND C WING)

Conceptual Design of Hybrid UAV

7. PRELIMINARY DESIGN OF A SINGLE AISLE MEDIUM RANGE AIRCRAFT

?????????? 24,??: Aug. 12, ulazca S. CoMA/asa BY) J. S. CONNER 2,425,306. Filed April 26, 1945 INVENTOR. 2 Sheets-Sheet l

Lockheed Martin. Team IDK Seung Soo Lee Ray Hernandez Chunyu PengHarshal Agarkar

Multi Engine Airplane Guide

European Aviation Safety Agency

COOPERATIVE PATENT CLASSIFICATION

RESEARCH MEMORANDUM. fox the. U. S. Air Force

Transcription:

Theory of Flight 6.01 Aircraft Design and Construction References: FTGU pages 9-14, 27 Main Teaching Points Parts of an Airplane Aircraft Construction Standard Terminology Definition The airplane is defined as: A power-driven Heavier-than air aircraft Deriving its lift in flight from aerodynamic reactions On surfaces that remain fixed under given conditions of flight. 1

Parts of an Airplane Parts of an Airplane Parts of an Airplane 2

Parts of an Airplane Fuselage The fuselage is the main body of the aircraft, where the passengers, cargo and crew go. Fuselage The fuselage is normally classified according to the type of construction: -Truss Type -Monocoque -Semi-monocoque 3

Fuselage Truss Type Fuselage Semi-Monocoque Empennage The empennage is the rear portion of the airplane It is integral to control and stability during flight 4

Wing Construction Spars spanwise members wood or metal carry bending loads Ribs web or truss give wing its cambered shape Wing Construction Edges Leading Edge Trailing Edge Strength & Shape Wires Internal / External Bracing for strength Covering Metal or Fabric Metal à strength Wing Layouts High Wing Mid Wing Low Wing Bi-Plane 5

17-10-27 Wing Layouts High Wing Mid Wing Low Wing Bi-Plane Wing Layouts High Wing Mid Wing Low Wing Bi-Plane Wing Layouts High Wing Mid Wing Low Wing Bi-Plane 6

Confirmation Conventional (Tail-Dragger) - Two main wheels and a tail wheel Tricycle Two main wheels and a nose wheel Retractable - Wheels may be raised so that they are enclosed in wings or fuselage (reducing drag) Fixed - Landing gear is not designed to retract 7

17-10-27 8

Retractable PROS Reduced drag at cruise Higher cruising speed CONS Added weight Added mechanical complexity Risk of Gear Up Landing (land based) Risk of Gear Down Landing (amphibious) Shock AbsorpIon Absorb the impact of landing, or the effect of bumps in runway. Spring steel Air/Oil oleos Rubber cords (bungee) or discs Low pressure Bres Main - Spring Steel Cantilever - 9

Nose - Air / Oil Oleo - Brakes - Brakes Provide a means of stopping the aircraq Assist with steering on the ground Confirmation How would you describe the aircraft to the left? -tail dragger? -tricycle gear? -retractable gear? -float plane? -high wing? -low wing? -mid wing? -biplane? Request the use of the tools to label the aircraft. 10

Wing Span Wingspan is the maximum distance from wing Bp to wing Bp Chord Chord is the imaginary line between the leading edge and the trailing edge of the wing A measure of the width of a wing Wing Area Wing Area Length of the wing multiplied by the average width of wing 11

Planform Planform Shape of the wing as seen from above Aspect Ratio Aspect RaBo RaIo of the span to chord of the wing A measure of how SLENDER the wing is Airfoil A structure curved to produce lift 12

Camber Camber A measure of the curvature of an airfoil Mean Camber is the line equidistant between the upper & lower surfaces Angle of Incidence Angle of Incidence Angle between chord line and the longitudinal axis RelaBve Airflow Relative Airflow Airflow over the wing Related to the forward moion of the aircraq through the air 13

Angle of Attack Angle of AXack The angle between the chord line and the relaive airflow It is a measure of how much the wing bites into the air Confirmation Check Confirmation Confirmation What kind of landing gear is this? 14

17-10-27 Confirmation What is the angle of attack? Confirmation What are some of the differences between powered aircraft and gliders? Confirmation Reading: From the Ground Up, pages 9-14 The next Theory of Flight Class covers the basic flight controls (6.02) 15