Theory and practice of aircraft performance /

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autores principales: Kundu, Ajoy Kumar, 1934- (Autor), Price, Mark (Aerospace engineer) (Autor), Riordan, David (Aerospace engineer) (Autor)
Formato: Electrónico eBook
Idioma:Inglés
Publicado: [Place of publication not identified] : Wiley, [2016]
Colección:Aerospace series (Chichester, England)
Temas:
Airplanes > Performance.
Avions > Performances.
Airplanes > Performance
Electronic books.
Acceso en línea:Texto completo
Texto completo
Tabla de Contenidos:
  • Title Page
  • Copyright Page
  • Contents
  • Preface
  • Series Preface
  • Road Map of the Book
  • Acknowledgements
  • Nomenclature
  • Chapter 1 Introduction
  • 1.1 Overview
  • 1.2 Brief Historical Background
  • 1.2.1 Flight in Mythology
  • 1.2.2 Fifteenth to Nineteenth Centuries
  • 1.2.3 From 1900 to World War I (1914)
  • 1.2.4 World War I (1914-1918)
  • 1.2.5 The Inter-War Period: the Golden Age (1918-1939)
  • 1.2.6 World War II (1939-1945)
  • 1.2.7 Post World War II
  • 1.3 Current Aircraft Design Status
  • 1.3.1 Current Civil Aircraft Trends
  • 1.3.2 Current Military Aircraft Trends
  • 1.4 Future Trends
  • 1.4.1 Trends in Civil Aircraft
  • 1.4.2 Trends in Military Aircraft
  • 1.4.3 Forces and Drivers
  • 1.5 Airworthiness Requirements
  • 1.6 Current Aircraft Performance Analyses Levels
  • 1.7 Market Survey
  • 1.8 Typical Design Process
  • 1.8.1 Four Phases of Aircraft Design
  • 1.9 Classroom Learning Process
  • 1.10 Cost Implications
  • 1.11 Units and Dimensions
  • 1.12 Use of Semi empirical Relations and Graphs
  • 1.13 How Do Aircraft Fly?
  • 1.13.1 Classification of Flight Mechanics
  • 1.14 Anatomy of Aircraft
  • 1.14.1 Comparison between Civil and Military Design Requirements
  • 1.15 Aircraft Motion and Forces
  • 1.15.1 Motion
  • Kinematics
  • 1.15.2 Forces
  • Kinetics
  • 1.15.3 Aerodynamic Parameters
  • Lift, Drag and Pitching Moment
  • 1.15.4 Basic Controls
  • Sign Convention
  • References
  • Chapter 2 Aerodynamic and Aircraft Design Considerations
  • 2.1 Overview
  • 2.2 Introduction
  • 2.3 Atmosphere
  • 2.3.1 Hydrostatic Equations and Standard Atmosphere
  • 2.3.2 Non-standard/Off-standard Atmosphere
  • 2.3.3 Altitude Definitions
  • Density Altitude (Off standard)
  • 2.3.4 Humidity Effects
  • 2.3.5 Greenhouse Gases Effect
  • 2.4 Airflow Behaviour: Laminar and Turbulent
  • 2.4.1 Flow Past an Aerofoil
  • 2.5 Aerofoil
  • 2.5.1 Subsonic Aerofoil.
  • 2.5.2 Supersonic Aerofoil
  • 2.6 Generation of Lift
  • 2.6.1 Centre of Pressure and Aerodynamic Centre
  • 2.6.2 Relation between Centre of Pressure and Aerodynamic Centre
  • 2.7 Types of Stall
  • 2.7.1 Buffet
  • 2.8 Comparison of Three NACA Aerofoils
  • 2.9 High-Lift Devices
  • 2.10 Transonic Effects
  • Area Rule
  • 2.10.1 Compressibility Correction
  • 2.11 Wing Aerodynamics
  • 2.11.1 Induced Drag and Total Aircraft Drag
  • 2.12 Aspect Ratio Correction of 2D-Aerofoil Characteristics for 3D-Finite Wing
  • 2.13 Wing Definitions
  • 2.13.1 Planform Area, SW
  • 2.13.2 Wing Aspect Ratio
  • 2.13.3 Wing-Sweep Angle
  • 2.13.4 Wing Root (croot) and Tip (ctip) Chords
  • 2.13.5 Wing-Taper Ratio, n
  • 2.13.6 Wing Twist
  • 2.13.7 High/Low Wing
  • 2.13.8 Dihedral/Anhedral Angles
  • 2.14 Mean Aerodynamic Chord
  • 2.15 Compressibility Effect: Wing Sweep
  • 2.16 Wing-Stall Pattern and Wing Twist
  • 2.17 Influence of Wing Area and Span on Aerodynamics
  • 2.17.1 The Square-Cube Law
  • 2.17.2 Aircraft Wetted Area (AW) versus Wing Planform Area (SW)
  • 2.17.3 Additional Wing Surface Vortex Lift
  • Strake/Canard
  • 2.17.4 Additional Surfaces on Wing
  • Flaps/Slats and High Lift Devices
  • 2.17.5 Other Additional Surfaces on Wing
  • 2.18 Empennage
  • 2.18.1 Tail-arm
  • 2.18.2 Horizontal Tail (H-Tail)
  • 2.18.3 Vertical Tail (V-Tail)
  • 2.18.4 Tail-Volume Coefficients
  • 2.19 Fuselage
  • 2.19.1 Fuselage Axis/Zero-Reference Plane
  • 2.19.2 Fuselage Length, Lfus
  • 2.19.3 Fineness Ratio, FR
  • 2.19.4 Fuselage Upsweep Angle
  • 2.19.5 Fuselage Closure Angle
  • 2.19.6 Front Fuselage Closure Length, Lf
  • 2.19.7 Aft Fuselage Closure Length, La
  • 2.19.8 Mid-Fuselage Constant Cross-Section Length, Lm
  • 2.19.9 Fuselage Height, H
  • 2.19.10 Fuselage Width, W
  • 2.19.11 Average Diameter, Dave
  • 2.20 Nacelle and Intake.
  • 2.20.1 Large Commercial/Military Logistic and Old Bombers Nacelle Group
  • 2.20.2 Small Civil Aircraft Nacelle Position
  • 2.20.3 Intake/Nacelle Group (Military Aircraft)
  • 2.20.4 Futuristic Aircraft Nacelle Positions
  • 2.21 Speed Brakes and Dive Brakes
  • References
  • Chapter 3 Air Data Measuring Instruments, Systems and Parameters
  • 3.1 Overview
  • 3.2 Introduction
  • 3.3 Aircraft Speed
  • 3.3.1 Definitions Related to Aircraft Velocity
  • 3.3.2 Theory Related to Computing Aircraft Velocity
  • 3.3.3 Aircraft Speed in Flight Deck Instruments
  • 3.3.4 Atmosphere with Wind Speed (Non-zero Wind)
  • 3.3.5 Calibrated Airspeed
  • 3.3.6 Compressibility Correction (EVc)
  • 3.3.7 Other Position Error Corrections
  • 3.4 Air Data Instruments
  • 3.4.1 Altitude Measurement
  • Altimeter
  • 3.4.2 Airspeed Measuring Instrument
  • Pitot-Static Tube
  • 3.4.3 Angle-of-Attack Probe
  • 3.4.4 Vertical Speed Indicator
  • 3.4.5 Temperature Measurement
  • 3.4.6 Turn-Slip Indicator
  • 3.5 Aircraft Flight-Deck (Cockpit) Layout
  • 3.5.1 Multifunctional Displays and Electronic Flight Information Systems
  • 3.5.2 Combat Aircraft Flight Deck
  • 3.5.3 Head-Up Display (HUD)
  • 3.6 Aircraft Mass (Weights) and Centre of Gravity
  • 3.6.1 Aircraft Mass (Weights) Breakdown
  • 3.6.2 Desirable CG Position
  • 3.6.3 Weights Summary
  • Civil Aircraft
  • 3.6.4 CG Determination
  • Civil Aircraft
  • 3.6.5 Bizjet Aircraft CG Location
  • Classroom Example
  • 3.6.6 Weights Summary
  • Military Aircraft
  • 3.6.7 CG Determination
  • Military Aircraft
  • 3.6.8 Classroom Worked Example
  • Military AJT CG Location
  • 3.7 Noise Emissions
  • 3.7.1 Airworthiness Requirements
  • 3.7.2 Summary
  • 3.8 Engine-Exhaust Emissions
  • 3.9 Aircraft Systems
  • 3.9.1 Aircraft Control System
  • 3.9.2 ECS: Cabin Pressurization and Air Conditioning
  • 3.9.3 Oxygen Supply.
  • 8.3 Uninstalled Turbofan Engine Performance Data
  • Civil Aircraft.

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