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

Size: px
Start display at page:

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

Transcription

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

2 Propulsion system options 2

3 Propulsion system options 3

4 Jet engine integration Engine dimensions: L=L nominal (SF) 0.4 D=D nominal (SF) 0.5 W=W nominal (SF) 1.1 SF =T req /T nominal 4

5 Turbofan engine dimensions 5

6 Inlet geometry 6

7 Inlet geometry An inlet must produce: A high pressure recovery (1% loss in inlet pressure recovery results in 1.3% loss in thrust). Deceleration so that the Mach # at the engine entrance is Low drag. 7

8 Inlet geometry There are four basic types of inlets: NACA inlet: reduced wetted surface area and weight but poor in pressure recovery. 8

9 Inlet geometry Pitot inlet: works well subsonically and fairly well at low supersonic speeds. However, the normal shock produced will reduce pressure recovery so it is not suitable for prolonged operation above M=1.4. 9

10 Inlet geometry Conical (spike or round) intake: exploits shock patterns created by the supersonic flow over a cone. The spike inlet is lighter and has slightly better pressure recovery but has higher cowl drag and mechanically more complex. Suitable for M>

11 Inlet geometry Ramp inlet: Uses the shock pattern produced by a wedge. Suitable for M<

12 Inlet location 12

13 Inlet location 13

14 Inlet location 14

15 Inlet location Inlet must not be placed where it can ingest a vortex off the fuselage or separated wake from the wing, the inlet flow distortion can stall the engine. The nose location offers the inlet a completely clean airflow, but requires a very long internal duct, which is heavy with high losses, requires high volume. The chin inlet has the advantage of a nose inlet with a shorter duct. It is particularly good at high α because the fuselage forebody helps to turn the flow into it. Nose landing gear must not be placed ahead of the inlet. Another problem is foreign object ingestion. 15

16 Inlet location For a low bypass ratio turbofan: vertical distance of the inlet from the ground should be > 80% of inlet height. For a high bypass ratio turbofan: vertical distance of the inlet from the ground should be > 50% of inlet height. 16

17 Capture area calculation Multiply capture area/mass flow by mass flow of the engine. 17

18 Propeller engine integration Propeller size: Function of propeller: take shaft power from the engine and convert it into thrust power. Propellers achieve this with some inevitable losses. η p = TV P < 1 Propeller efficiency as diameter of propeller due to lower accelaration through the disk. The larger the propeller, the higher the mass of air processed by it. 18

19 Propeller engine integration For the same thrust, a larger diameter propeller requires a smaller velocity increase accross the propeller disc. Smaller the velocity increase in any propulsive device, the higher the propulsive efficiency. 19

20 Propeller engine integration Two constraints for the propeller: The propeller tip must clear the ground when the airplane is on the ground. Propeller tip speed should be less than the speed of sound, otherwise compressibility effects will ruin the propeller performance. At the same time, the propeller must be large enough to absorb engine power. The power absorption of the propeller is increased by increasing the diameter and/or increasing the number of blades. 20

21 Propeller tip speed V tip,static = πnd, N: rotational speed, d: diameter of propeller V tip,helical = 2 V tip,static + V 2, V : flight speed At sea level, the helical tip speed of a metal propeller < 950 ft/s At sea level, the helical tip speed of a wooden propeller < 850 ft/s If noise is a concern, V tip,helical < 700 ft/s during takeoff. 21

22 Blade diameter Two blades: d = hp, Three blades: d = hp Four + blades: d = hp The propeller diameters from the two approaches are compared and the smaller of the two is selected. 22

23 Blade diameter Advantages of two blades: Less weight, Higher efficiency due to higher diameter. Advantages of three or four blades: Smaller diameter, shorter landing gear, Less severe compressibility effects, Higher efficiency due to better power absorption. 23

24 Propeller location 24

25 Propeller location 25

26 Propeller location Alternatives: Tractor: puts the heavy engine to the front, shortening the forebody. This allows a smaller tail area and improves stability. Also provides a ready source of cooling air and the propeller is placed in undisturbed air. Pusher: it reduces skin friction drag because the airplane flies in undisturbed air. It also reduces wetted area by shortening the fuselage. The inlow caused by the propeller accelerates the air over the fuselage, delaying flow separation. However, the pusher configuration has reduced propeller efficiency because it encounters disturbed air off the fuselage, wings, etc. Since the heavy engine is at the rear, the tail must be larger for stability. The pusher propeller may require a longer landing gear for propeller clearance during takeoff or landing. 26

27 Propeller location Alternatives: Wing mounted: is normally used for multi-engine designs. Reduces fuselage drag by removing the fuselage from the propeller wake. However, introduces engine-out controllability problems due to asymmetrical thrust enlarging the size of the vertical tail and the rudder. The propeller tip must be at lesat 9 of the ground at all attitudes. The crew compartment should not be located within ±5 o of the propeller disc. 27

28 Propeller location 28

29 Propeller location 29

30 Engine size estimation An existing engine can be scaled using scaling equations: X scaled = X nominal SF b, X: weight, length, diameter. 30

31 Engine size estimation Alternatively, statistical models can be used. 31

32 In-line engine 32

33 Radial engine 33

34 Fuel system Fuel system includes: Fuel tanks only components effecting overall aircraft layout. Fuel lines. Fuel pumps. Fuel management controls. 34

35 Fuel system There three types of fuel tanks: Discrete: fuel containers that are separately fabricated and mounted in the aircraft by bolts. Normally, used only for general aviation and homebuilt airplanes. Bladder: is made by stuffing a shaped rubber bag into a cavity in the structure. Available fuel volume is decreased by 10% because of rubber thickness. Self sealing. Integral: cavities within the airframe structure that are sealed to form a fuel tank. May be created simply by sealing a wing-box or cavities between two fuselage bulkheads. 35

36 Fuel system The required volume of the fuel tanks is based on total required fuel calculated during initial sizing. 36

37 Fuel system 37

38 Fuel system Rules of thumb: 85 % of the volume measured to the external skin surface is usable for integral wing tanks. 92 % of the volume measured to the external skin surface is usable for integral fuselage tanks. 77 % for wing and 83 % for fuselage of the volume is usable in bladder tanks. Allow for 3-5% extra volume to account for fuel expansion on hot days. 38

AE 452 Aeronautical Engineering Design II Installed Engine Performance. Prof. Dr. Serkan Özgen Dept. Aerospace Engineering March 2016

AE 452 Aeronautical Engineering Design II Installed Engine Performance. Prof. Dr. Serkan Özgen Dept. Aerospace Engineering March 2016 AE 452 Aeronautical Engineering Design II Installed Engine Performance Prof. Dr. Serkan Özgen Dept. Aerospace Engineering March 2016 Propulsion 2 Propulsion F = ma = m V = ρv o S V V o ; thrust, P t =

More information

In this lecture... Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay

In this lecture... Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay 1 In this lecture... Intakes for powerplant Transport aircraft Military aircraft 2 Intakes Air intakes form the first component of all air breathing propulsion systems. The word Intake is normally used

More information

Aeronautical Engineering Design II Sizing Matrix and Carpet Plots. Prof. Dr. Serkan Özgen Dept. Aerospace Engineering Spring 2014

Aeronautical Engineering Design II Sizing Matrix and Carpet Plots. Prof. Dr. Serkan Özgen Dept. Aerospace Engineering Spring 2014 Aeronautical Engineering Design II Sizing Matrix and Carpet Plots Prof. Dr. Serkan Özgen Dept. Aerospace Engineering Spring 2014 Empty weight estimation and refined sizing Empty weight of the airplane

More information

Prof. João Melo de Sousa Instituto Superior Técnico Aerospace & Applied Mechanics. Part B Acoustic Emissions 4 Airplane Noise Sources

Prof. João Melo de Sousa Instituto Superior Técnico Aerospace & Applied Mechanics. Part B Acoustic Emissions 4 Airplane Noise Sources Prof. João Melo de Sousa Instituto Superior Técnico Aerospace & Applied Mechanics Part B Acoustic Emissions 4 Airplane Noise Sources The primary source of noise from an airplane is its propulsion system.

More information

AE 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 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 information

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

AE 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 information

AE Aircraft Performance and Flight Mechanics

AE Aircraft Performance and Flight Mechanics AE 429 - Aircraft Performance and Flight Mechanics Propulsion Characteristics Types of Aircraft Propulsion Mechanics Reciprocating engine/propeller Turbojet Turbofan Turboprop Important Characteristics:

More information

Chapter 4 Estimation of wing loading and thrust loading - 10 Lecture 18 Topics

Chapter 4 Estimation of wing loading and thrust loading - 10 Lecture 18 Topics Chapter 4 Estimation of wing loading and thrust loading - 10 Lecture 18 Topics 4.15.3 Characteristics of a typical turboprop engine 4.15.4 Characteristics of a typical turbofan engine 4.15.5 Characteristics

More information

SR-71 PROPULSION SYSTEM P&W J58 ENGINE (JT11D-20) ONE OF THE BEST JET ENGINES EVER BUILT

SR-71 PROPULSION SYSTEM P&W J58 ENGINE (JT11D-20) ONE OF THE BEST JET ENGINES EVER BUILT SR-71 PROPULSION SYSTEM P&W J58 ENGINE (JT11D-20) PETER LAW ONE OF THE BEST JET ENGINES EVER BUILT Rolls-Royce Milestone Engines Merlin Conway W2B Welland Derwent Trent SR-71 GENERAL CHARACTERISTICS

More information

General Dynamics F-16 Fighting Falcon

General 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 information

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

Aircraft 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 information

AERONAUTICAL ENGINEERING

AERONAUTICAL 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 information

Welcome to Aerospace Engineering

Welcome to Aerospace Engineering Welcome to Aerospace Engineering DESIGN-CENTERED INTRODUCTION TO AEROSPACE ENGINEERING Notes 5 Topics 1. Course Organization 2. Today's Dreams in Various Speed Ranges 3. Designing a Flight Vehicle: Route

More information

ENGINE STARTING PERFORMANCE EVALUATION AT STATIC STATE CONDITIONS USING SUPERSONIC AIR INTAKE

ENGINE STARTING PERFORMANCE EVALUATION AT STATIC STATE CONDITIONS USING SUPERSONIC AIR INTAKE 24 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES STARTING PERFORMANCE EVALUATION AT STATIC STATE CONDITIONS USING SUPERSONIC AIR INTAKE Author1* Takashi Nishikido Author2* Iwao Murata Author3**

More information

Chapter 4 Lecture 16. Engine characteristics 4. Topics. Chapter IV

Chapter 4 Lecture 16. Engine characteristics 4. Topics. Chapter IV Chapter 4 Lecture 16 Engine characteristics 4 Topics 4.3.3 Characteristics of a typical turboprop engine 4.3.4 Characteristics of a typical turbofan engine 4.3.5 Characteristics of a typical turbojet engines

More information

Aircraft Propulsion Technology

Aircraft Propulsion Technology Unit 90: Aircraft Propulsion Technology Unit code: L/601/7249 QCF level: 4 Credit value: 15 Aim This unit aims to develop learners understanding of the principles and laws of aircraft propulsion and their

More information

Propeller blade shapes

Propeller blade shapes 31 1 Propeller blade shapes and Propeller Tutorials 2 Typical Propeller Blade Shape 3 M Flight M. No. Transonic Propeller Airfoil 4 Modern 8-bladed propeller with transonic airfoils near the tip and swept

More information

1.1 REMOTELY PILOTED AIRCRAFTS

1.1 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 information

Chapter 10 Miscellaneous topics - 2 Lecture 39 Topics

Chapter 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 information

Reducing Landing Distance

Reducing Landing Distance Reducing Landing Distance I've been wondering about thrust reversers, how many kinds are there and which are the most effective? I am having a debate as to whether airplane engines reverse, or does something

More information

Felix Du Temple de la Croix Monoplane 1857

Felix Du Temple de la Croix Monoplane 1857 2 1 Felix Du Temple de la Croix Monoplane 1857 2 Thrust for Flight 3 Unpowered airplanes George Cayle s design (early 19 th century) Samuel P Langley s Airplane (late 19 th century) 4 Langley s Airplane

More information

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

Systems 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 information

Preface. Acknowledgments. List of Tables. Nomenclature: organizations. Nomenclature: acronyms. Nomenclature: main symbols. Nomenclature: Greek symbols

Preface. Acknowledgments. List of Tables. Nomenclature: organizations. Nomenclature: acronyms. Nomenclature: main symbols. Nomenclature: Greek symbols Contents Preface Acknowledgments List of Tables Nomenclature: organizations Nomenclature: acronyms Nomenclature: main symbols Nomenclature: Greek symbols Nomenclature: subscripts/superscripts Supplements

More information

Supersonic Combustion Experimental Investigation at T2 Hypersonic Shock Tunnel

Supersonic Combustion Experimental Investigation at T2 Hypersonic Shock Tunnel Supersonic Combustion Experimental Investigation at T2 Hypersonic Shock Tunnel D. Romanelli Pinto, T.V.C. Marcos, R.L.M. Alcaide, A.C. Oliveira, J.B. Chanes Jr., P.G.P. Toro, and M.A.S. Minucci 1 Introduction

More information

CHAPTER 1 AIRCRAFT GENERAL

CHAPTER 1 AIRCRAFT GENERAL CHAPTER 1 AIRCRAFT GENERAL INTRODUCTION This manual provides a description of the major airframe and engine systems in the Cessna Citation Mustang (Figure 1-1). This material does not supersede, nor is

More information

European Aviation Safety Agency

European Aviation Safety Agency Page 1 of 9 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET APM 20 and APM 30 series Type Certificate Holder: BP 1 Manufacturer: BP 1 For variants: APM 20 APM 30 Issue 3 : 23 December

More information

In this lecture... Fixed and variable geometry nozzles Functions of nozzles Thrust vector control Thrust reversal Noise control

In this lecture... Fixed and variable geometry nozzles Functions of nozzles Thrust vector control Thrust reversal Noise control 1 In this lecture... Nozzle: Fixed and variable geometry nozzles Functions of nozzles Thrust vector control Thrust reversal Noise control 2 Exhaust nozzles Nozzles form the exhaust system of gas turbine

More information

INDIAN INSTITUTE OF TECHNOLOGY KANPUR

INDIAN INSTITUTE OF TECHNOLOGY KANPUR INDIAN INSTITUTE OF TECHNOLOGY KANPUR INDIAN INSTITUTE OF TECHNOLOGY KANPUR Removable, Low Noise, High Speed Tip Shape Tractor Configuration, Cant angle, Low Maintainence Hingelesss, Good Manoeuverability,

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: 1.2. What

More information

The Airplane That Could!

The 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 information

Introduction to Aerospace Engineering

Introduction to Aerospace Engineering Introduction to Aerospace Engineering Lecture slides Challenge the future 1 18-9-2011 Introduction to Aerospace Engineering AE1101ab - Propulsion Delft University of Technology Prof.dr.ir. Challenge JaccotheHoekstra

More information

Turbo-Rocket. A brand new class of hybrid rocket. Rene Nardi and Eduardo Mautone

Turbo-Rocket. A brand new class of hybrid rocket. Rene Nardi and Eduardo Mautone Turbo-Rocket R A brand new class of hybrid rocket Rene Nardi and Eduardo Mautone 53 rd AIAA/SAE/ASEE Joint Propulsion Conference July 10 12, 2017 - Atlanta, Georgia Rumo ao Espaço R - UFC Team 2 Background

More information

European Aviation Safety Agency

European Aviation Safety Agency Page 1/8 European Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET Cirrus Design SF50 Type Certificate Holder: Cirrus Design Corporation 4515 Taylor Circle Duluth, Minnesota 55811 United States

More information

Ultralight airplane Design

Ultralight 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 information

Lect-28. In this lecture...

Lect-28. In this lecture... 1 In this lecture... Lect-28 Performance of intakes Performance parameters Sources of losses Starting problem in supersonic intakes Modes of operation of an external compression intake 2 Intake performance

More information

LAD Inc. Beechcraft King Air 200 Series Technical Ground School Syllabus Material Covered

LAD Inc. Beechcraft King Air 200 Series Technical Ground School Syllabus Material Covered Topic Introduction Description Structures ATA 05 Technical Publications ATA 05 Aircraft Handling ATA 12 LAD Inc. Beechcraft King Air 200 Series Technical Ground School Syllabus Material Covered Course

More information

Click to edit Master title style

Click to edit Master title style AVIATION OPERATIONAL MEASURES FOR FUEL AND EMISSIONS REDUCTION WORKSHOP Fuel Conservation Third Airframe level Maintenance for Environmental Performance Dave Anderson Flight Operations Engineer Boeing

More information

ELECTRIC POWER TRAINS THE KEY ENABLER FOR CONTRA ROTATING PROPELLERS IN GENERAL AVIATION (& VICE VERSA)

ELECTRIC POWER TRAINS THE KEY ENABLER FOR CONTRA ROTATING PROPELLERS IN GENERAL AVIATION (& VICE VERSA) ELECTRIC POWER TRAINS THE KEY ENABLER FOR CONTRA ROTATING PROPELLERS IN GENERAL AVIATION (& VICE VERSA) ATI D3 EVENT 8 TH MAY 2018 THE EMERGENCE OF ELECTRIFICATION IN AEROSPACE NICK SILLS, CONTRA ELECTRIC

More information

Y. Lemmens, T. Benoit, J. de Boer, T. Olbrechts LMS, A Siemens Business. Real-time Mechanism and System Simulation To Support Flight Simulators

Y. Lemmens, T. Benoit, J. de Boer, T. Olbrechts LMS, A Siemens Business. Real-time Mechanism and System Simulation To Support Flight Simulators Y. Lemmens, T. Benoit, J. de Boer, T. Olbrechts LMS, A Siemens Business Real-time Mechanism and System Simulation To Support Flight Simulators Smarter decisions, better products. Contents Introduction

More information

Methodology for Distributed Electric Propulsion Aircraft Control Development with Simulation and Flight Demonstration

Methodology for Distributed Electric Propulsion Aircraft Control Development with Simulation and Flight Demonstration 1 Methodology for Distributed Electric Propulsion Aircraft Control Development with Simulation and Flight Demonstration Presented by: Jeff Freeman Empirical Systems Aerospace, Inc. jeff.freeman@esaero.com,

More information

FLASHCARDS AIRCRAFT. Courtesy of the Air Safety Institute, a Division of the AOPA Foundation, and made possible by AOPA Services Corporation.

FLASHCARDS AIRCRAFT. Courtesy of the Air Safety Institute, a Division of the AOPA Foundation, and made possible by AOPA Services Corporation. AIRCRAFT FLASHCARDS Courtesy of the Air Safety Institute, a Division of the AOPA Foundation, and made possible by AOPA Services Corporation. Knowing your aircraft well is essential to safe flying. These

More information

Concept study Propulsive Fuselage

Concept study Propulsive Fuselage Concept study Propulsive Fuselage 75% Reduction 90% Reduction Increase of installed seats 2009 to 2035 (ACI Forecast 2009) Increase of aircraft movements 2009 to 2035 (ACI Forecast 2009) The European Commission

More information

(VTOL) Propulsion Systems Design

(VTOL) Propulsion Systems Design 72-GT-73 $3.00 PER COPY $1.00 TO ASME MEMBERS The Society shall not be responsible for statements or opinions advanced in papers or in discussion at meetings of the Society or of its Divisions or Sections,

More information

SR-71 Inlet Design Issues And Solutions Dealing With Behaviorally Challenged Supersonic Flow Systems

SR-71 Inlet Design Issues And Solutions Dealing With Behaviorally Challenged Supersonic Flow Systems SR-71 Inlet Design Issues And Solutions Dealing With Behaviorally Challenged Supersonic Flow Systems 3/4/14 Tom Anderson 1 A-12, SR-71 Inlet Designers Dave Campbell SR-71 Inlet Designer Propulsion Boss

More information

AIRCRAFT DESIGN SUBSONIC JET TRANSPORT

AIRCRAFT 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 information

XIV.C. Flight Principles Engine Inoperative

XIV.C. Flight Principles Engine Inoperative XIV.C. Flight Principles Engine Inoperative References: FAA-H-8083-3; POH/AFM Objectives The student should develop knowledge of the elements related to single engine operation. Key Elements Elements Schedule

More information

Aircraft Design Conceptual Design

Aircraft 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 information

TAKEOFF PERFORMANCE ground roll

TAKEOFF PERFORMANCE ground roll TAKEOFF PERFORMANCE An airplane is motionless at the end of a runway. This is denoted by location O. The pilot releases the brakes and pushes the throttle to maximum takeoff power, and the airplane accelerates

More information

Here is the gap seal I used for the flaps, genuine hardware store quality. Note cross sectional shape visible on the right end.

Here is the gap seal I used for the flaps, genuine hardware store quality. Note cross sectional shape visible on the right end. HOMEBUILT AIRCRAFT DRAG REDUCTION - Case Study with a Lancair IV Part 3 Copyright - Fred Moreno - January 2009 Rev. 1 Portions may be reproduced for private, individual use 3- REDUCED AIRFRAME DRAG FOR

More information

Preliminary Detailed Design Review

Preliminary 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 information

The Sonic Cruiser A Concept Analysis

The Sonic Cruiser A Concept Analysis International Symposium "Aviation Technologies of the XXI Century: New Aircraft Concepts and Flight Simulation", 7-8 May 2002 Aviation Salon ILA-2002, Berlin The Sonic Cruiser A Concept Analysis Dr. Martin

More information

Owners Manual. Table of Contents 3.1. INTRODUCTION AIRSPEEDS FOR EMERGENCY OPERATION OPERATIONAL CHECKLISTS 3

Owners Manual. Table of Contents 3.1. INTRODUCTION AIRSPEEDS FOR EMERGENCY OPERATION OPERATIONAL CHECKLISTS 3 EMERGENCY PROCEDURES Table of Contents 3.1. INTRODUCTION 2 3.2. AIRSPEEDS FOR EMERGENCY OPERATION 2 3.3. OPERATIONAL CHECKLISTS 3 3.3.1. ENGINE FAILURES 3. ENGINE FAILURE DURING TAKEOFF RUN 3. ENGINE FAILURE

More information

Jump to Table of Contents

Jump to Table of Contents Jump to Table of Contents PIPER AIRCRAFT CORPORATION PA-28R-201, CHEROKEE ARROW III SECTION 3 EMERGENCY PROCEDURES 3.3 EMERGENCY PROCEDURES CHECK LIST ENGINE FIRE DURING

More information

Aircraft Design in a Nutshell

Aircraft Design in a Nutshell Dieter Scholz Aircraft Design in a Nutshell Based on the Aircraft Design Lecture Notes 1 Introduction The task of aircraft design in the practical sense is to supply the "geometrical description of a new

More information

AN ADVANCED COUNTER-ROTATING DISK WING AIRCRAFT CONCEPT Program Update. Presented to NIAC By Carl Grant November 9th, 1999

AN ADVANCED COUNTER-ROTATING DISK WING AIRCRAFT CONCEPT Program Update. Presented to NIAC By Carl Grant November 9th, 1999 AN ADVANCED COUNTER-ROTATING DISK WING AIRCRAFT CONCEPT Program Update Presented to NIAC By Carl Grant November 9th, 1999 DIVERSITECH, INC. Phone: (513) 772-4447 Fax: (513) 772-4476 email: carl.grant@diversitechinc.com

More information

Design of a High Altitude Fixed Wing Mini UAV Aerodynamic Challenges

Design of a High Altitude Fixed Wing Mini UAV Aerodynamic Challenges Design of a High Altitude Fixed Wing Mini UAV Aerodynamic Challenges Hemant Sharma 1, C. S. Suraj 2, Roshan Antony 3, G. Ramesh 4, Sajeer Ahmed 5 and Prasobh Narayan 6 1, 2, 3, 4 CSIR National Aerospace

More information

Jet Aircraft Propulsion Prof. Bhaskar Roy Prof. A.M. Pradeep Department of Aerospace Engineering Indian Institute of Technology, Bombay

Jet Aircraft Propulsion Prof. Bhaskar Roy Prof. A.M. Pradeep Department of Aerospace Engineering Indian Institute of Technology, Bombay Jet Aircraft Propulsion Prof. Bhaskar Roy Prof. A.M. Pradeep Department of Aerospace Engineering Indian Institute of Technology, Bombay Lecture No. # 04 Turbojet, Reheat Turbojet and Multi-Spool Engines

More information

Design Considerations for Stability: Civil Aircraft

Design 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 information

Robot Dynamics Rotary Wing UAS: Introduction, Mechanical Design and Aerodynamics

Robot Dynamics Rotary Wing UAS: Introduction, Mechanical Design and Aerodynamics Robot Dynamics Rotary Wing UAS: Introduction, Mechanical Design and Aerodynamics 151-0851-00 V Marco Hutter, Michael Blösch, Roland Siegwart, Konrad Rudin and Thomas Stastny Robot Dynamics: Rotary Wing

More information

Design Rules and Issues with Respect to Rocket Based Combined Cycles

Design Rules and Issues with Respect to Rocket Based Combined Cycles Respect to Rocket Based Combined Cycles Tetsuo HIRAIWA hiraiwa.tetsuo@jaxa.jp ABSTRACT JAXA Kakuda space center has been studying rocket based combined cycle engine for the future space transportation

More information

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

Flugzeugentwurf / 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 information

SILENT SUPERSONIC TECHNOLOGY DEMONSTRATION PROGRAM

SILENT SUPERSONIC TECHNOLOGY DEMONSTRATION PROGRAM 25 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES SILENT SUPERSONIC TECHNOLOGY DEMONSTRATION PROGRAM Akira Murakami* *Japan Aerospace Exploration Agency Keywords: Supersonic, Flight experiment,

More information

Hawker Beechcraft Corporation on March 26, 2007

Hawker Beechcraft Corporation on March 26, 2007 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A00010WI Revision 8 Hawker Beechcraft 390 March 26, 2007 TYPE CERTIFICATE DATA SHEET NO. A00010WI This data sheet, which is part of Type Certificate

More information

Airframes Instructor Training Manual. Chapter 6 UNDERCARRIAGE

Airframes 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 information

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

MD 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 information

JODEL D.112 INFORMATION MANUAL C-FVOF

JODEL 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 information

Future Trends in Aeropropulsion Gas Turbines

Future Trends in Aeropropulsion Gas Turbines Future Trends in Aeropropulsion Gas Turbines Cyrus B. Meher-Homji, P.E. Turbomachinery Group Bechtel Corporation ASME SW Texas Gas Turbine Technical Chapter 12-Nov-2012 Copyright 2012 : C.B. Meher-Homji

More information

DEVELOPMENT OF A CARGO AIRCRAFT, AN OVERVIEW OF THE PRELIMINARY AERODYNAMIC DESIGN PHASE

DEVELOPMENT OF A CARGO AIRCRAFT, AN OVERVIEW OF THE PRELIMINARY AERODYNAMIC DESIGN PHASE ICAS 2000 CONGRESS DEVELOPMENT OF A CARGO AIRCRAFT, AN OVERVIEW OF THE PRELIMINARY AERODYNAMIC DESIGN PHASE S. Tsach, S. Bauminger, M. Levin, D. Penn and T. Rubin Engineering center Israel Aircraft Industries

More information

Preflight Inspection Cabin EMPENNAGE RIGHT WING Trailing Edge RIGHT WING NOSE

Preflight Inspection Cabin EMPENNAGE RIGHT WING Trailing Edge RIGHT WING NOSE Preflight Inspection Cabin 1. Control Wheel Lock REMOVED 2. Ignition Switch OFF 3. Avionics Power Switch OFF 4. Master Switch ON 5. Fuel Quantity Indicators CHECK QUANTITY 6. Master Switch OFF 7. Fuel

More information

Propulsion Controls and Diagnostics Research at NASA GRC Status Report

Propulsion Controls and Diagnostics Research at NASA GRC Status Report Propulsion Controls and Diagnostics Research at NASA GRC Status Report Dr. Sanjay Garg Branch Chief Ph: (216) 433-2685 FAX: (216) 433-8990 email: sanjay.garg@nasa.gov http://www.lerc.nasa.gov/www/cdtb

More information

Lecture 5 : Static Lateral Stability and Control. or how not to move like a crab. G. Leng, Flight Dynamics, Stability & Control

Lecture 5 : Static Lateral Stability and Control. or how not to move like a crab. G. Leng, Flight Dynamics, Stability & Control Lecture 5 : Static Lateral Stability and Control or how not to move like a crab 1.0 Lateral static stability Lateral static stability refers to the ability of the aircraft to generate a yawing moment to

More information

EAS 4700 Aerospace Design 1

EAS 4700 Aerospace Design 1 EAS 4700 Aerospace Design 1 Prof. P.M. Sforza University of Florida Commercial Airplane Design 1 1.Mission specification and market survey Number of passengers: classes of service Range: domestic or international

More information

Cessna 172RG WARNING. Maximum Demonstrated Crosswind. Takeoff or landing..15 KTS

Cessna 172RG WARNING. Maximum Demonstrated Crosswind. Takeoff or landing..15 KTS Cessna 172RG INTRODUCTION: This aircraft checklist contains information from the original manufacturer s Pilot Information Manual. Normal procedures associated with optional systems can be found in Section

More information

TABLE OF CONTENTS. Chapter 1: AIRCRAFT - GENERAL Chapter 2: ELECTRICAL SYSTEM Chapter 3: ANNUNCIATOR SYSTEM...37

TABLE OF CONTENTS. Chapter 1: AIRCRAFT - GENERAL Chapter 2: ELECTRICAL SYSTEM Chapter 3: ANNUNCIATOR SYSTEM...37 TABLE OF CONTENTS Chapter 1: AIRCRAFT - GENERAL... 4 Chapter 2: ELECTRICAL SYSTEM...21 Chapter 3: ANNUNCIATOR SYSTEM...37 Chapter 4: FUEL SYSTEM...43 Chapter 5: ENGINE SYSTEM...60 Chapter 6: PROPELLER

More information

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

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

More information

Jay Gundlach AIAA EDUCATION SERIES. Manassas, Virginia. Joseph A. Schetz, Editor-in-Chief. Blacksburg, Virginia. Aurora Flight Sciences

Jay Gundlach AIAA EDUCATION SERIES. Manassas, Virginia. Joseph A. Schetz, Editor-in-Chief. Blacksburg, Virginia. Aurora Flight Sciences Jay Gundlach Aurora Flight Sciences Manassas, Virginia AIAA EDUCATION SERIES Joseph A. Schetz, Editor-in-Chief Virginia Polytechnic Institute and State University Blacksburg, Virginia Published by the

More information

FLOW CHARACTERIZATION FROM A NACA AIR INTAKE ASSEMBLED IN A CANARD TYPE AIRCRAFT

FLOW CHARACTERIZATION FROM A NACA AIR INTAKE ASSEMBLED IN A CANARD TYPE AIRCRAFT FLOW CHARACTERIZATION FROM A NACA AIR INTAKE ASSEMBLED IN A CANARD TYPE AIRCRAFT O. de Almeida, and P. R. C. Souza Centro de Pesquisa em Aerodinâmica Experimental - CPAERO Faculdade de Engenharia Mecânica

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A49NM

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A49NM DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A49NM Jetcruzer 450 June 14, 1994 TYPE CERTIFICATE DATA SHEET NO. A49NM This data sheet which is a part of Type Certificate A49NM, prescribes

More information

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

MD - 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 information

L 298/70 Official Journal of the European Union

L 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 information

FLIGHT TEST RESULTS AT TRANSONIC REGION ON SUPERSONIC EXPERIMENTAL AIRPLANE (NEXST-1)

FLIGHT TEST RESULTS AT TRANSONIC REGION ON SUPERSONIC EXPERIMENTAL AIRPLANE (NEXST-1) 26 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES FLIGHT TEST RESULTS AT TRANSONIC REGION ON SUPERSONIC EXPERIMENTAL AIRPLANE (NEXST-1) Dong-Youn Kwak*, Hiroaki ISHIKAWA**, Kenji YOSHIDA* *Japan

More information

New Design Concept of Compound Helicopter

New 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 information

PAC 750XL PAC 750XL PAC-750XL

PAC 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 information

Powertrain Design for Hand- Launchable Long Endurance Unmanned Aerial Vehicles

Powertrain 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 information

Aeroplane Aerodynamics and Flight Controls 1 2

Aeroplane 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 information

INCORPORA:1EO. PO Box Shannon Lane Priest River, FAA APPROVED

INCORPORA:1EO. PO Box Shannon Lane Priest River, FAA APPROVED INCORPORA:1EO FAA APPROVED Document A-1 0023.., Page 1 of. 9 Rev, (see rev. page) SUPPLEMENTAL AIRPLANE FLIGHT MANUAL FOR CESSNA 180J & 180K SERIES FLOATPLANES Modified with Kenmore Air Harbor STC # SA649NW

More information

On-Demand Mobility Electric Propulsion Roadmap

On-Demand Mobility Electric Propulsion Roadmap On-Demand Mobility Electric Propulsion Roadmap Mark Moore, ODM Senior Advisor NASA Langley Research Center EAA AirVenture, Oshkosh July 22, 2015 NASA Distributed Electric Propulsion Research Rapid, early

More information

Weight Effects Part 1

Weight Effects Part 1 Weight Effects Part 1 David F. Rogers Copyright c 1997-1999 David F. Rogers. All rights reserved. Most of us normally operate our aircraft at less than gross weight, yet weight significantly affects the

More information

Sample. Module 17A and 17B Licence Category A, B1 and B3. Propeller Fundamentals. Module 17 Propeller. Copyright 2014 Total Training Support Ltd

Sample. Module 17A and 17B Licence Category A, B1 and B3. Propeller Fundamentals. Module 17 Propeller. Copyright 2014 Total Training Support Ltd Module 17A and 17B Licence Category A, B1 and B3 Propeller 17.1 Fundamentals Module 17.1 Fundamentals Page 1 Copyright Notice Copyright. All worldwide rights reserved. No part of this publication may be

More information

AIAA Undergraduate Team Aircraft Design

AIAA Undergraduate Team Aircraft Design Homeland Defense Interceptor (HDI) 2005 2006 AIAA Undergraduate Team Aircraft Design Group Members and Responsibilities Name Discipline AIAA Number John Borgie Configuration and Systems 268357 Ron Cook

More information

CNY Rocket Team Challenge. Basics of Using RockSim 9 to Predict Altitude for the Central New York Rocket Team Challenge

CNY Rocket Team Challenge. Basics of Using RockSim 9 to Predict Altitude for the Central New York Rocket Team Challenge CNY Rocket Team Challenge Basics of Using RockSim 9 to Predict Altitude for the Central New York Rocket Team Challenge RockSim 9 Basics 2 Table of Contents A. Introduction.p. 3 B. Designing Your Rocket.p.

More information

Electric VTOL Aircraft

Electric VTOL Aircraft Electric VTOL Aircraft Subscale Prototyping Overview Francesco Giannini fgiannini@aurora.aero 1 08 June 8 th, 2017 Contents Intro to Aurora Motivation & approach for the full-scale vehicle Technical challenges

More information

ERA's Open Rotor Studies Including Shielding For Noise Reduction Environmentally Responsible Aviation Project

ERA's Open Rotor Studies Including Shielding For Noise Reduction Environmentally Responsible Aviation Project National Aeronautics and Space Administration ERA's Open Rotor Studies Including Shielding For Noise Reduction Environmentally Responsible Aviation Project Dale Van Zante and Russell Thomas Presented by:

More information

Multidisciplinary Design Optimization for a Blended Wing Body Transport Aircraft with Distributed Propulsion

Multidisciplinary Design Optimization for a Blended Wing Body Transport Aircraft with Distributed Propulsion Multidisciplinary Design Optimization for a Blended Wing Body Transport Aircraft with Distributed Propulsion Leifur Thor Leifsson, Andy Ko, William H. Mason, Joseph A. Schetz, Raphael T. Haftka, and Bernard

More information

AIRCRAFT AND TECHNOLOGY CONCEPTS FOR AN N+3 SUBSONIC TRANSPORT. Elena de la Rosa Blanco May 27, 2010

AIRCRAFT AND TECHNOLOGY CONCEPTS FOR AN N+3 SUBSONIC TRANSPORT. Elena de la Rosa Blanco May 27, 2010 AIRCRAFT AND TECHNOLOGY CONCEPTS FOR AN N+3 SUBSONIC TRANSPORT MIT, Aurora Flights Science, and Pratt & Whitney Elena de la Rosa Blanco May 27, 2010 1 The information in this document should not be disclosed

More information

Landing Gear Layout Design for Unmanned Aerial Vehicle

Landing Gear Layout Design for Unmanned Aerial Vehicle Landing Gear Layout Design for Unmanned Aerial Vehicle Akhilesh Jha SDET Division, ADE/DRDO, Bangalore, India Corresponding author (email: akhilsdet@yahoo.com) Abstract Aircraft landing gear mechanism

More information

CARENADO COPYRIGHTS. Normal & Emergency Checklist

CARENADO COPYRIGHTS. Normal & Emergency Checklist NORMAL PROCEDURES CHECKLIST PREFLIGHT CHECK Control wheel -- RELEASE BELTS Avionics -- OFF Master Switch -- ON Fuel quantity gauges -- CHECK Master switch -- OFF Ignition -- OFF Exterior -- CHECK FOR DAMAGE

More information

Chapter 4 Engine characteristics (Lectures 13 to 16)

Chapter 4 Engine characteristics (Lectures 13 to 16) Chapter 4 Engine characteristics (Lectures 13 to 16) Keywords: Engines for airplane applications; piston engine; propeller characteristics; turbo-prop, turbofan and turbojet engines; choice of engine for

More information

NASA centers team up to tackle sonic boom 18 March 2014, by Frank Jennings, Jr.

NASA centers team up to tackle sonic boom 18 March 2014, by Frank Jennings, Jr. NASA centers team up to tackle sonic boom 18 March 2014, by Frank Jennings, Jr. This rendering shows the Lockheed Martin future supersonic advanced concept featuring two engines under the wings and one

More information

TYPE-CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET TYPE-CERTIFICATE DATA SHEET NO. EASA.IM.A.073 for Beechcraft 390 (PREMIER I and IA) Type Certificate Holder: Textron Aviation Inc. One Cessna Boulevard Wichita, Kansas 67215 USA For Models: Model 390 1

More information