Theory of Flight. Main Teaching Points. Definition Parts of an Airplane Aircraft Construction Landing Gear Standard Terminology
|
|
- Milton Lamb
- 5 years ago
- Views:
Transcription
1 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
2 Parts of an Airplane Parts of an Airplane Parts of an Airplane 2
3 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
4 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
5 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
6 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
7 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
8
9 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
10 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
11 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
12 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
13 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
14 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
15 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
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: 1.2. What
More informationAircraft Maintenance Prof. A.K Ghosh Prof. Vipul Mathur Department of Aerospace Engineering Indian Institute of Technology, Kanpur
Aircraft Maintenance Prof. A.K Ghosh Prof. Vipul Mathur Department of Aerospace Engineering Indian Institute of Technology, Kanpur Lecture 05 Aircraft Landing Gear System Now, coming to the next aircraft
More informationSD3-60 AIRCRAFT MAINTENANCE MANUAL. This chapter includes information on dimensions, areas, zoning, etc. and is presented as follows:
AMM 6-00-00 1.0.0.0GENERAL 1. General This chapter includes information on dimensions, areas, oning, etc. and is presented as follows: Measurements and Figures which show the stations of fuselage frames,
More informationPreliminary Detailed Design Review
Preliminary Detailed Design Review Project Review Project Status Timekeeping and Setback Management Manufacturing techniques Drawing formats Design Features Phase Objectives Task Assignment Justification
More informationMD RA Minister's Delegates - Recreational Aviation Représentants du Ministre - Aviation de loisir
Think Safety Pensons Securite MD RA Minister's Delegates - Recreational Aviation Représentants du Ministre - Aviation de loisir Inspection Service Service d'inspection MDRA C20 MANUAL of PROCEDURES for
More informationThe Airplane That Could!
The Airplane That Could! Critical Design Review December 6 th, 2008 Haoyun Fu Suzanne Lessack Andrew McArthur Nicholas Rooney Jin Yan Yang Yang Agenda Criteria Preliminary Designs Down Selection Features
More informationMD - RA. Minister s Delegates - Recreational Aviation Représentants du Ministre - Aviation de Loisir Service d Inspection
Think Safety Inspection Service MD - RA Pensons Sécurité Minister s Delegates - Recreational Aviation Représentants du Ministre - Aviation de Loisir Service d Inspection 51% Amateur Determination Checklist
More informationCHAPTER 10. WEIGHT AND BALANCE
9/27/01 AC 43.13-1B CHG 1 CHAPTER 10. WEIGHT AND BALANCE SECTION 1 TERMINOLOGY 10-1. GENERAL. The removal or addition of equipment results in changes to the center of gravity (c.g.). The empty weight of
More informationCONCEPTUAL DESIGN OF ECOLOGICAL AIRCRAFT FOR COMMUTER AIR TRANSPORTATION
26 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES CONCEPTUAL DESIGN OF ECOLOGICAL AIRCRAFT FOR COMMUTER AIR TRANSPORTATION Yasuhiro TANI, Tomoe YAYAMA, Jun-Ichiro HASHIMOTO and Shigeru ASO Department
More informationFUNDAMENTALS OF ROTOR AND POWER TRAIN MAINTENANCE TECHNIQUES AND PROCEDURES
FUNDAMENTALS OF ROTOR AND POWER TRAIN MAINTENANCE TECHNIQUES AND PROCEDURES DISTRIBUTION RESTRICTION: Approved for public release; distribution is unlimited. HEADQUARTERS, DEPARTMENT OF THE ARMY CHAPTER
More informationAIRCRAFT DESIGN SUBSONIC JET TRANSPORT
AIRCRAFT DESIGN SUBSONIC JET TRANSPORT Analyzed by: Jin Mok Professor: Dr. R.H. Liebeck Date: June 6, 2014 1 Abstract The purpose of this report is to design the results of a given specification and to
More informationPAC 750XL PAC 750XL PAC-750XL
PAC 750XL The PAC 750XL combines a short take off and landing performance with a large load carrying capability. The PAC 750XL is a distinctive type. Its design philosophy is reflected in the aircraft's
More informationAircraft Design Conceptual Design
Université de Liège Département d Aérospatiale et de Mécanique Aircraft Design Conceptual Design Ludovic Noels Computational & Multiscale Mechanics of Materials CM3 http://www.ltas-cm3.ulg.ac.be/ Chemin
More informationAERONAUTICAL ENGINEERING
AERONAUTICAL ENGINEERING SHIBIN MOHAMED Asst. Professor Dept. of Mechanical Engineering Al Ameen Engineering College Al- Ameen Engg. College 1 Aerodynamics-Basics These fundamental basics first must be
More informationState of Israel Ministry of Transport Civil Aviation Authority TYPE CERTIFICATE DATA SHEET
State of Israel Ministry of Transport Civil Aviation Authority TYPE CERTIFICATE DATA SHEET TC number: Revision: Aircraft make: Aircraft model: IA298 New BRM Aero BRISTELL RG This Data Sheet which is part
More informationAE 451 Aeronautical Engineering Design Final Examination. Instructor: Prof. Dr. Serkan ÖZGEN Date:
Instructor: Prof. Dr. Serkan ÖZGEN Date: 11.01.2012 1. a) (8 pts) In what aspects an instantaneous turn performance is different from sustained turn? b) (8 pts) A low wing loading will always increase
More informationDesign, Build, Fly Q&A #1
2018-19 Design, Build, Fly Q&A #1 Fuselage 1. How do you define a fuselage? How is underneath or bottom of the fuselage defined? Answer: The fuselage is defined as the main body of the airplane that is
More informationAircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 3 Aircraft Conceptual Design. Tables
Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 3 Aircraft Conceptual Design Tables No Component Primary function Major areas of influence 1 Fuselage Payload accommodations
More informationUltralight airplane Design
Ultralight airplane Design Ultralight airplane definitions: Airworthiness authorities define aircraft as vehicles that can rise or move in the air and enforce strict regulations and requirements for all
More informationAircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 11 Aircraft Weight Distribution Tables
Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 01 Chapter 11 Aircraft Weight Distribution Tables No Component group Elements Weight X cg Y cg Z cg 1 Wing 1.1. Wing main structure 1..
More informationProp effects (Why we need right thrust) Torque reaction Spiraling Slipstream Asymmetric Loading of the Propeller (P-Factor) Gyroscopic Precession
Prop effects (Why we need right thrust) Torque reaction Spiraling Slipstream Asymmetric Loading of the Propeller (P-Factor) Gyroscopic Precession Propeller torque effect Influence of engine torque on aircraft
More informationAmendment List. Crown Copyright 2007
No Amendment List Date Amended by Date Incorporated 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 Crown Copyright 2007 i ACP 33 FLIGHT CONTENTS Volume 1...History of Flight Volume 2...Principles of Flight Volume
More informationSIMULATION OF PROPELLER EFFECT IN WIND TUNNEL
SIMULATION OF PROPELLER EFFECT IN WIND TUNNEL J. Červinka*, R. Kulhánek*, Z. Pátek*, V. Kumar** *VZLÚ - Aerospace Research and Test Establishment, Praha, Czech Republic **C-CADD, CSIR-NAL, Bangalore, India
More informationNew Design Concept of Compound Helicopter
New Design Concept of Compound Helicopter PRASETYO EDI, NUKMAN YUSOFF and AZNIJAR AHMAD YAZID Department of Engineering Design & Manufacture, Faculty of Engineering, University of Malaya, 50603 Kuala Lumpur,
More informationDUCHESS BE-76 AND COMMERCIAL MULTI ADD-ON ORAL REVIEW FOR CHECKRIDE
DUCHESS BE-76 AND COMMERCIAL MULTI ADD-ON ORAL REVIEW FOR CHECKRIDE The Critical Engine The critical engine is the engine whose failure would most adversely affect the airplane s performance or handling
More informationSAE Aero Design. Mid-point Review 3/10/2016. By Ali Alqalaf, Jasem Alshammari, Dong Yang Cao, Darren Frankenberger, Steven Goettl, and John Santoro
SAE Aero Design Mid-point Review By Ali Alqalaf, Jasem Alshammari, Dong Yang Cao, Darren Frankenberger, Steven Goettl, and John Santoro 3/10/2016 Overview Introduction Problem Definition Need Statement
More informationDesign Considerations for Stability: Civil Aircraft
Design Considerations for Stability: Civil Aircraft From the discussion on aircraft behavior in a small disturbance, it is clear that both aircraft geometry and mass distribution are important in the design
More informationAE 440: Conceptual Design Report for the Agricultural Unmanned Aircraft System. X Duster: XD 44X
AE 440: Conceptual Design Report for the Agricultural Unmanned Aircraft System X Duster: XD 44X Aerodynamics and Team Leader: Timothy Lingner Configuration: Matthew Fuesz Cost and Components: Wesley Hammes
More informationA SOLAR POWERED UAV. 1 Introduction. 2 Requirements specification
A SOLAR POWERED UAV Students: R. al Amrani, R.T.J.P.A. Cloosen, R.A.J.M. van den Eijnde, D. Jong, A.W.S. Kaas, B.T.A. Klaver, M. Klein Heerenbrink, L. van Midden, P.P. Vet, C.J. Voesenek Project tutor:
More informationFlugzeugentwurf / Aircraft Design SS Part 35 points, 70 minutes, closed books. Prof. Dr.-Ing. Dieter Scholz, MSME. Date:
DEPARTMENT FAHRZEUGTECHNIK UND FLUGZEUGBAU Flugzeugentwurf / Aircraft Design SS 2015 Duration of examination: 180 minutes Last Name: Matrikelnummer: First Name: Prof. Dr.-Ing. Dieter Scholz, MSME Date:
More informationAIRCRAFT DESIGN MADE EASY. Basic Choices and Weights. By Chris Heintz
AIRCRAFT DESIGN MADE EASY By Chris Heintz The following article, which is a first installement of a two-part article, describes a simple method for the preliminary design of an airplane of conventional
More informationSystems Group (Summer 2012) 4 th Year (B.Eng) Aerospace Engineering Candidate Carleton University, Ottawa,Canada Mail:
Memo Airport2030_M_Family_Concepts_of_Box_Wing_12-08-10.pdf Date: 12-08-10 From: Sameer Ahmed Intern at Aero Aircraft Design and Systems Group (Summer 2012) 4 th Year (B.Eng) Aerospace Engineering Candidate
More information2014 SAE AERO DESIGN EAST COMPETITION 10% Report
EML 4905 Senior Design Project A B.S. THESIS PREPARED IN PARTIAL FULFILLMENT OF THE REQUIREMENT FOR THE DEGREE OF BACHELOR OF SCIENCE IN MECHANICAL ENGINEERING 2014 SAE AERO DESIGN EAST COMPETITION 10%
More informationBuilding A Replica Aircraft. Part Three Construction Details Wings and Covering
Building A Replica Aircraft Part Three Construction Details Wings and Covering The human brain is a wonderful organ. It starts to work as soon as you are born and doesn't stop until you get up to deliver
More informationINVESTIGATION OF ICING EFFECTS ON AERODYNAMIC CHARACTERISTICS OF AIRCRAFT AT TSAGI
INVESTIGATION OF ICING EFFECTS ON AERODYNAMIC CHARACTERISTICS OF AIRCRAFT AT TSAGI Andreev G.T., Bogatyrev V.V. Central AeroHydrodynamic Institute (TsAGI) Abstract Investigation of icing effects on aerodynamic
More informationFUSELAGE ASSEMBLY SECOND SECTION (of three)
FUSELAGE ASSEMBLY SECOND SECTION (of three) 1 FRONT FLOOR ASSEMBLY The front floor assembly is fabricated from three pieces of the two ply pre-pregnated panel material supplied. The basic floor panel and
More informationTHE SAGRES PROJECT - A NEW VERY LIGHT AEROPLANE. Department of Aerospace Sciences Universidade da Beira Interior Covilhã, Portugal
THE SAGRES PROJECT - A NEW VERY LIGHT AEROPLANE Ivan A. Camelier * & Pedro V. Gamboa Department of Aerospace Sciences Universidade da Beira Interior Covilhã, Portugal Abstract This project aims at designing
More informationPowertrain Design for Hand- Launchable Long Endurance Unmanned Aerial Vehicles
Powertrain Design for Hand- Launchable Long Endurance Unmanned Aerial Vehicles Stuart Boland Derek Keen 1 Justin Nelson Brian Taylor Nick Wagner Dr. Thomas Bradley 47 th AIAA/ASME/SAE/ASEE JPC Outline
More informationEuropean Aviation Safety Agency
Page 1 of 7 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.045 Type Certificate Holder: Blanik Aircraft CZ s.r.o. Karolinská 661/4 186 00 Praha 8 For models: Issue 05: 10 January
More informationCONCEPTUAL DESIGN REPORT
CONCEPTUAL DESIGN REPORT Agricultural Unmanned Aircraft System (AUAS) Team Two-CAN Team Member Albert Lee (Team Leader) Chris Cirone Kevin Huckshold Adam Kuester Jake Niehus Michael Scott Area of Responsibility
More informationEuropean Aviation Safety Agency
TCDS EASA.IM.A.162 Page 1/9 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Tupolev TU 204-120CE Manufacturer: Tupolev PSC 17, Tupolev Embankment 111250 Moscow Russia For model: TU 204-120CE
More informationAircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, Chapter 9 Landing Gear Design. Figures
Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 9 Landing Gear Design Figures cg strut wheel Main gear Height (H) Wheel base (B) cg Height (H) Wheel track (T) Figure 9.1.
More information1.1 REMOTELY PILOTED AIRCRAFTS
CHAPTER 1 1.1 REMOTELY PILOTED AIRCRAFTS Remotely Piloted aircrafts or RC Aircrafts are small model radiocontrolled airplanes that fly using electric motor, gas powered IC engines or small model jet engines.
More informationEuropean Aviation Safety Agency
European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET VSO 10 Type Certificate Holder: Schempp-Hirth výroba letadel spol. s r.o U Dvořiska 1733 565 01 Choceň EASA TCDS No. A.442 For variants:
More informationThis 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
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 product at the time it was written. We can't speak for
More informationFlying Wing. Matt Statzer Bryan Williams Mike Zauberman. 17 March
Flying Wing http://www.nurflugel.com/nurflugel/northrop/n-1m/n1m_refurbished_1.jpg Matt Statzer Bryan Williams Mike Zauberman http://www.geocities.com/witewings/bwb/gallerydetail-1-6.html 17 March 2003
More information2iJ AIRO2AFT CIRCTJLARS. THE GLOSTER "GAMBET t AIRPLANE. A Deck-Lding Ship's Fighter. Fitted with a 420 HP. Bristol Jupiter VI Engine
LE 2iJ COPY AIRO2AFT CIRCTJLARS HATIONAL ADVISORY COAMITTEE FOR RONAUTICS ITo. 48 THE GLOSTER "GAMBET t AIRPLANE A Deck-Lding Ship's Fighter Fitted with a 420 HP. Bristol Jupiter VI Engine ashington July,
More informationAirframes Instructor Training Manual. Chapter 6 UNDERCARRIAGE
Learning Objectives Airframes Instructor Training Manual Chapter 6 UNDERCARRIAGE 1. The purpose of this chapter is to discuss in more detail the last of the Four Major Components the Undercarriage (or
More informationAMT 111 Aircraft Landing Gear Systems. Chapter 13
AMT 111 Aircraft Landing Gear Systems Chapter 13 Complex Hard Working Big Small Hard Core Landing Gear Arrangement Tail Wheel/Tail Dragger/Conventional Tricycle Tandem v Gliders or Military Floats v Amphibious
More informationSAE Aero Design. Apr 29, 2016
SAE Aero Design Ali Alqalaf, Jasem Alshammari, Dong Yang Cao, Darren Frankenberger, Steven Goettl, and John Santoro Department of Mechanical Engineering Apr 29, 2016 Overview Introduction Need Statement
More informationMooney Mite M-18X Plans and Drawings Index Arranged by Group Miscellaneous Group
Miscellaneous Group 110470 Bushings - Special 314410 Airspeed & Altimeter Installation 110190 Arm - Landing Warning 110070 Button - Static Airspeed 213260 Cone - Wing Fillet 110120 Control - Placard 616100
More information4.1 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
4.0 GROUND MANEUVERING 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 4.6 Runway Holding Bay DECEMBER 2002
More informationL 298/70 Official Journal of the European Union
L 298/70 Official Journal of the European Union 16.11.2011 MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS 12.1 Theory of Flight Rotary Wing Aerodynamics 1 2 Terminology; Effects of gyroscopic
More informationAeroplane Aerodynamics and Flight Controls 1 2
11.1 Theory of Flight 11.1.1. Aeroplane Aerodynamics and Flight Controls 1 2 Operation and effect of: roll control: ailerons and spoilers, pitch control: elevators, stabilators, variable incidence stabilisers
More informationSD3-60 STRUCTURAL REPAIR MANUAL
SRM 1.0.0.0STRUCTURES - GENERAL 1. Introduction This chapter contains structural repair information of a general nature pertaining to the complete aircraft. Areas particularly prone to damage are shown.
More informationGeneral Dynamics F-16 Fighting Falcon
General Dynamics F-16 Fighting Falcon http://www.globalsecurity.org/military/systems/aircraft/images/f-16c-19990601-f-0073c-007.jpg Adam Entsminger David Gallagher Will Graf AOE 4124 4/21/04 1 Outline
More informationEuropean Aviation Safety Agency
TCDS A.006 Tecnam P2002 Page 1 of 12 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET P2002 Manufacturer: Costruzioni Aeronautiche TECNAM S.r.l. Costruzioni Aeronautiche TECNAM S.r.l. Via
More informationAVRO LANCASTER by Ivan Pettigrew Construction Notes
AVRO LANCASTER by Ivan Pettigrew Construction Notes For ease of transportation, the model may be built with the wing in three sections. The sections are held together with nylon clips. Assembly at the
More informationChapter No matter how you paint it, it s still going to roll, pitch and yaw. Identify Name Describe Identify Explain Describe Identify Describe
Chapter 8 Aircraft, spacecraft and even submarines (in a limited way) are capable of moving in all possible directions. That is, if one considers such craft to be suspended at the center of an imaginary
More informationAE 451 Aeronautical Engineering Design I Estimation of Critical Performance Parameters. Prof. Dr. Serkan Özgen Dept. Aerospace Engineering Fall 2015
AE 451 Aeronautical Engineering Design I Estimation of Critical Performance Parameters Prof. Dr. Serkan Özgen Dept. Aerospace Engineering Fall 2015 Airfoil selection The airfoil effects the cruise speed,
More informationAgricultural Unmanned Aircraft System (AUAS)
Agricultural Unmanned Aircraft System (AUAS) Team Two-CAN Albert Lee (TL) Jacob Niehus Adam Kuester Chris Cirone Michael Scott Kevin Huckshold 1 Presentation Overview Configuration Selection (KH) Initial
More informationMultidisciplinary Design Optimization of a Truss-Braced Wing Aircraft with Tip-Mounted Engines
Multidisciplinary Design Optimization of a Truss-Braced Wing Aircraft with Tip-Mounted Engines NASA Design MAD Center Advisory Board Meeting, November 14, 1997 Students: J.M. Grasmeyer, A. Naghshineh-Pour,
More information2.2 Schedule
Table of Contents 1.0 Executive Summary------------------------------------------------------------3 2.0 Management Summary--------------------------------------------------------4 2.1 Team Organization-----------------------------------------------------4
More informationAircraft Characteristics/ Aircraft Recognition
Aircraft Characteristics/ Aircraft Recognition 3-15-11 Aircraft Characteristics and Recognition 1 Lesson Objectives 1. Identify aircraft using common recognition features A. Categories. B. Weight classes.
More informationDESIGN OF A FIFTH GENERATION AIR SUPERIORITY FIGHTER AIRCRAFT
Proceedings of the International Conference on Mechanical Engineering and Renewable Energy 2015 (ICMERE2015) 26 29 November, 2015, Chittagong, Bangladesh ICMERE2015PI152 DESIGN OF A FIFTH GENERATION AIR
More informationUncontrolled copy not subject to amendment. Airframes. Revision 1.00
Uncontrolled copy not subject to amendment Airframes Revision 1.00 Chapter 4: Fuselage Learning Objectives The purpose of this chapter is to discuss in more detail the first of the 4 major components
More informationJODEL D.112 INFORMATION MANUAL C-FVOF
JODEL D.112 INFORMATION MANUAL C-FVOF Table of Contents I General Description...4 Dimensions:...4 Powertrain:...4 Landing gear:...4 Control travel:...4 II Limitations...5 Speed limits:...5 Airpeed indicator
More information12.1 Theory of Flight Rotary Wing Aerodynamics 1 2
12.1 Theory of Flight Rotary Wing Aerodynamics 1 2 Terminology; Effects of gyroscopic precession; Torque reaction and directional control; Dissymmetry of lift, Blade tip stall; Translating tendency and
More informationIrkut Corporation plant is manufacturing fuselage sections and carries out its assembly
MC-21 MC-21 is a perspective commercial aircraft with a capacity of 150 to 211 passengers. Irkut Corporation (a UAC company) is creating the plane within a wide international cooperation First aircraft
More informationAE 451 Aeronautical Engineering Design I Propulsion and Fuel System Integration. Prof. Dr. Serkan Özgen Dept. Aerospace Engineering December 2017
AE 451 Aeronautical Engineering Design I Propulsion and Fuel System Integration Prof. Dr. Serkan Özgen Dept. Aerospace Engineering December 2017 Propulsion system options 2 Propulsion system options 3
More informationA Game of Two: Airbus vs Boeing. The Big Guys. by Valerio Viti. Valerio Viti, AOE4984, Project #1, March 22nd, 2001
A Game of Two: Airbus vs Boeing The Big Guys by Valerio Viti 1 Why do we Need More Airliners in the Next 20 Years? Both Boeing and Airbus agree that civil air transport will keep increasing at a steady
More informationThank you again, Jim McCormick. Jabiru Pacific LLC
Thank you for your inquiry about Jabiru Aircraft. Jabiru Aircraft PTY, Ltd, produces a line of kit aircraft that are among the most extensively tested and thoroughly developed kit planes in the entire
More informationTowards the Optimisation of. Adaptive Aeroelastic Structures
Towards the Optimisation of Jonathan Cooper Mike Amprikidis, Vijaya Hodere, Gareth Vio School of Mechanical, Aerospace and Civil Engineering University of Manchester ERCOFTAC 6th April 2006 Contents Introduction
More informationSection 2: Basic Aerobatics
Section 2: Basic Aerobatics Airplane Considerations and Control Setup Primary to Aerobatic Airplane Transition Parallel Positioning B-34 Basic Aerobatics Introduction Aerobatics is unarguably the most
More informationHumming Aerospace Version 9 Blade ti
Humming Aerospace Version 9 Blade ti Designed By J Falk Hummingair LLC The Version 9 is a prototype carbon fiber intensive aircraft designed from the nose back to be much more efficient than existing aircraft
More informationAIRCRAFT CIRCULARS TATIOTAL ADVISORY COMMITTEE FOR AERONAUTICS. No A One-Place Cantilever Low-Wing Monoplane
I AIRCRAFT CIRCULARS TATIOTAL ADVISORY COMMITTEE FOR AERONAUTICS No. 144 THE 11 1.A.R." PURSUIT AIRPLANE (RouANIAN) A One-Place Cantilever Low-Wing Monoplane Washington May, 1931 NATIONAL ADVISORY CO}!iLITTEE
More informationDESIGN OF AN ARMAMENT WING FOR A LIGHT CATEGORY HELICOPTER
International Journal of Engineering Applied Sciences and Technology, 7 Published Online February-March 7 in IJEAST (http://www.ijeast.com) DESIGN OF AN ARMAMENT WING FOR A LIGHT CATEGORY HELICOPTER Miss.
More informationInstruction Manual EXTRA 260-EP. 1075mm (42.32 in) 1000mm (39.37 in) 1100gr gr. 4 channel - 4 mini servo. Axi motor 2820
1075mm (42.32 in) 1000mm (39.37 in) 1100gr - 1400gr 4 channel - 4 mini servo Axi motor 2820 KIT CONTENTS: We have organized the parts as they come out of the box for better identification during assembly.
More informationSAE BRAZIL AERODESIGN COMPETITION Final Report
EML 4905 Senior Design Project A B.S. THESIS PREPARED IN PARTIAL FULFILLMENT OF THE REQUIREMENT FOR THE DEGREE OF BACHELOR OF SCIENCE IN MECHANICAL ENGINEERING SAE BRAZIL AERODESIGN COMPETITION Final Report
More informationSAE Aero East 2017 Mid-Term Report
Mid-Term Report MAE 435W Project Management Project Advisor: Dr. Drew Landman Team Members: Sarah Arms, Aaron Calkins, David Ewing, Andy Helmann, Stacey LeGrand Mark Michielsen, Jordan Roque, Tonya White
More informationChapter 9 Landing Gear Design Mohammad Sadraey Daniel Webster College
Chapter 9 Landing Gear Design Mohammad Sadraey Daniel Webster College Table of Contents Chapter 9... 3 Landing Gear Design... 3 9.1. Introduction... 3 9.. Design Requirements and Design Flowchart... 4
More informationDesign of Ultralight Aircraft
Design of Ultralight Aircraft Greece 2018 Main purpose of present study The purpose of this study is to design and develop a new aircraft that complies with the European ultra-light aircraft regulations
More informationECO-CARGO AIRCRAFT. ISSN: International Journal of Science, Engineering and Technology Research (IJSETR) Volume 1, Issue 2, August 2012
ECO-CARGO AIRCRAFT Vikrant Goyal, Pankhuri Arora Abstract- The evolution in aircraft industry has brought to us many new aircraft designs. Each and every new design is a step towards a greener tomorrow.
More informationUnited States Patent (19) Cronk et al.
United States Patent (19) Cronk et al. (S4) LANDING GEAR FOR ULTRALIGHT AIRCRAFT 76) Inventors: David Cronk, 1069 Eucalyptus Ave., Vista, Calif. 92025; Lyle M. Byrum, 1471 Calle Redonda, Escondido, Calif.
More informationChapter 10 Miscellaneous topics - 2 Lecture 39 Topics
Chapter 10 Miscellaneous topics - 2 Lecture 39 Topics 10.3 Presentation of results 10.3.1 Presentation of results of a student project 10.3.2 A typical brochure 10.3 Presentation of results At the end
More information2000/2001 AIAA Foundation Cessna/ONR Student Design Build Fly Competition. Design Report Proposal Phase
2000/2001 AIAA Foundation Cessna/ONR Student Design Build Fly Competition Design Report Proposal Phase A Utah State University March 2001 Table of Contents Page # 1. Executive Summary...2 1.1 Conceptual
More informationAnalyzing Numerical Data: Using Ratios I.B Student Activity Sheet 5: Changing Tires
You have just purchased a new vehicle equipped with factory-installed P245/70R16 tires. You think these tires look too small, so you replace them with P285/75R16 tires. How does this change in tire size
More informationEuropean Aviation Safety Agency
TCDS A.185 Tecnam P2006T Page 1 of 8 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET P2006T Type Certificate Holder: Costruzioni Aeronautiche TECNAM S.r.l. Via Tasso, 478 80127 Napoli
More informationStrix Goblin Instruction Manual. Rev
Strix Goblin Instruction Manual Rev 3-4.24.2017 1 Introduction Thank you for purchasing the Strix Goblin! This is a high performance plank style aircraft and it was designed using aerodynamic principles
More informationChapter 2 Lecture 5 Data collection and preliminary three-view drawing - 2 Topic
Chapter 2 Lecture 5 Data collection and preliminary three-view dra - 2 Topic 2.3 Preliminary three-view dra Example 2.1 2.3 Preliminary three-view dra The preliminary three-view dra of the airplane gives
More informationRetro. An artist rendering inspired this great 40-size sport model BY BOB NOLL AND KEN MARONI 16 MODEL AVIATION
An artist rendering inspired this great 40-size sport model AGS Retro Photos by the author BY BOB NOLL AND KEN MARONI THIS IS THE story of a little sky-blue model that became famous even before it learned
More informationLAA TYPE ACCEPTANCE DATA SHEET TADS 193 RANS S4 AND RANS S5 (B WING AND C WING)
Issue 2 MOD/193/006 added, ref tail bracing wire tang cracking. dated 13.06.07 1. UK contact Skycraft Ltd., Kestrel, Broadgate, Weston Hills, Spalding. Lincs. PE12 6DP. United Kingdom Telephone: 01406
More informationConceptual Design of Hybrid UAV
ISSN (Online): 2394-3858 ISSN (Print) : 2394-3866 International Journal of Research and Innovations in Science & Technology, SAINTGITS College of Engineering, INDIA www.journals.saintgits.org Research
More information7. PRELIMINARY DESIGN OF A SINGLE AISLE MEDIUM RANGE AIRCRAFT
7. PRELIMINARY DESIGN OF A SINGLE AISLE MEDIUM RANGE AIRCRAFT Students: R.M. Bosma, T. Desmet, I.D. Dountchev, S. Halim, M. Janssen, A.G. Nammensma, M.F.A.L.M. Rommens, P.J.W. Saat, G. van der Wolf Project
More information?????????? 24,??: Aug. 12, ulazca S. CoMA/asa BY) J. S. CONNER 2,425,306. Filed April 26, 1945 INVENTOR. 2 Sheets-Sheet l
Aug. 12, 1947. J. S. CONNER RETRACTILE WING AND ANDING GEAR Filed April 26, 1945 2 Sheets-Sheet l INVENTOR. ulazca S. CoMA/asa BY)?????????? 24,??: Aug. 12, 1947, J. S. CONNER RETRACTILE WING AND LANDING
More informationLockheed Martin. Team IDK Seung Soo Lee Ray Hernandez Chunyu PengHarshal Agarkar
Lockheed Martin Team IDK Seung Soo Lee Ray Hernandez Chunyu PengHarshal Agarkar Abstract Lockheed Martin has developed several different kinds of unmanned aerial vehicles that undergo harsh forces when
More informationMulti Engine Airplane Guide
Multi Engine Airplane Guide Tecnam P2006T TABLE OF CONTENTS Introduction to Multi Engine Aircraft... 1 V Speeds... 2 Performance and Limitations... 4 Engine Ceilings... 4 Single Engine Climb Performance...
More informationEuropean Aviation Safety Agency
TCDS IM.A.080 BD100-1A10 (Challenger 300) Page 1/11 Issue 3.0, 26 October 2010 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET IM.A.080 CHALLENGER 300 Manufacturer: BOMBARDIER INC. P.
More informationCOOPERATIVE PATENT CLASSIFICATION
CPC B COOPERATIVE PATENT CLASSIFICATION PERFORMING OPERATIONS; TRANSPORTING (NOTES omitted) TRANSPORTING B64 AIRCRAFT; AVIATION; COSMONAUTICS AEROPLANES; HELICOPTERS (air-cushion vehicles B60V) NOTE As
More informationRESEARCH MEMORANDUM. fox the. U. S. Air Force
RESEARCH MEMORANDUM fox the U. S. Air Force - NACA RM SL53L24 NATIONAL ADVISORY COMMITTEE FOR AERONAIJTICS RESEARCH "ORANDUM the for U. S. Air Force _.I SPEED-BRAKE INVESTIGATION AT LOW SPEEDOF A l/lo-scale
More information