Cover -- Title Page -- Copyright Page -- Contents -- Preface -- Aerospace Series Preface -- Chapter 1 A Simple Flight Model -- 1.1 Introduction -- 1.1.1 General Introduction to Volume 2 -- 1.1.2 What Chapter 1 Includes -- 1.1.3 What Chapter 1 Excludes -- 1.1.4 Overall Aim -- 1.2 Flight Path -- 1.3 Flight Environment < -- 20 km -- 1.4 Simple Propulsion Model -- 1.4.1 Reference Parameters -- 1.4.2 Simple Jet Engine Performance -- 1.4.3 'Better' Jet Engine Performance -- 1.4.4 Simple Jet Engine Dynamics -- 1.5 Simple Aerodynamic Model -- 1.5.1 Idealised Aircraft -- 1.5.2 Idealised Wing -- 1.5.3 Wing/Tail Combination -- 1.5.4 Lift Distribution -- 1.5.5 Adding Flight Controls -- 1.6 Airspeed Definitions -- 1.7 Flight Model Architecture -- Chapter 2 Equations of Motion -- 2.1 Introduction -- 2.1.1 The Problem with Equations of Motion -- 2.1.2 What Chapter 2 Includes -- 2.1.3 What Chapter 2 Excludes -- 2.1.4 Overall Aim -- 2.2 Spatial Reference Model -- 2.2.1 Generic Reference Frames -- 2.2.2 Rotating Reference Frames -- 2.2.3 Elementary Rotations -- 2.2.4 Reference Frames for Position and Orientation -- 2.2.5 Reference Frame for Flight Path -- 2.2.6 Airspeed and Airstream Direction -- 2.3 Aircraft Dynamics -- 2.3.1 Mass Properties -- 2.3.2 Flight Parameters -- 2.3.3 Dynamic Equations of Motion -- 2.4 Aircraft Kinematics -- 2.4.1 Aircraft Position -- 2.4.2 Quaternions -- 2.4.3 Kinematic Equations of Motion -- 2.5 Initialisation -- 2.5.1 Balancing Forces -- 2.5.2 Typical Flight Conditions -- 2.5.3 Finding Aircraft Flight Parameters for Equilibrium -- 2.6 Linearisation -- 2.6.1 Linearisation of Dynamic Equations of Motion -- 2.6.2 Linearisation of Kinematic Equations of Motion -- 2.6.3 Linearisation of Aerodynamic Forces and Moments -- 2.6.4 Linearisation of Propulsive Forces and Moments -- 2.6.5 Linearisation of Gravitational Forces and Moments.

2.6.6 The Complete Linearised System of Equations -- Chapter 3 Fixed-Wing Aerodynamics -- 3.1 Introduction -- 3.1.1 Fixed Wings and Aerodynamics -- 3.1.2 What Chapter 3 Includes -- 3.1.3 What Chapter 3 Excludes -- 3.1.4 Overall Aim -- 3.2 Aerodynamic Principles -- 3.2.1 Aerofoils -- 3.2.2 Dimensional Analysis -- 3.2.3 Lift, Drag, and Pitching Moment -- 3.2.4 Aerodynamic Centre -- 3.2.5 Wing Geometry -- 3.2.6 NACA Four-Digit Sections -- 3.3 Aerodynamic Model of an Isolated Wing -- 3.3.1 Aerodynamic Lift -- 3.3.2 Pitching Moment -- 3.3.3 Drag Force -- 3.3.4 Profile Drag -- 3.3.5 Induced Drag -- 3.3.6 Wave Drag -- 3.4 Trailing-Edge Controls -- 3.4.1 Incremental Lift -- 3.4.2 Incremental Drag -- 3.4.3 Incremental Pitching Moment -- 3.4.4 Hinge Moments -- 3.5 Factors affecting Lift Generation -- 3.5.1 Sideslip -- 3.5.2 Aircraft Rotation -- 3.5.3 Structural Flexibility -- 3.5.4 Ground Effect -- 3.5.5 Indicial Aerodynamics -- 3.6 Lift Distribution -- 3.7 Drag Distribution -- Chapter 4 Longitudinal Flight -- 4.1 Introduction -- 4.1.1 Flight with Wings Level -- 4.1.2 What Chapter 4 Includes -- 4.1.3 What Chapter 4 Excludes -- 4.1.4 Overall Aim -- 4.2 Aerodynamic Fundamentals -- 4.3 Geometry -- 4.4 Wing/Body Combination -- 4.4.1 Lift Force -- 4.4.2 Downwash -- 4.4.3 Pitching Moment -- 4.4.4 Aerodynamic Centre -- 4.4.5 Drag Force -- 4.5 All-Moving Tail -- 4.5.1 Lift Force -- 4.5.2 Pitching Moment -- 4.5.3 Drag Force -- 4.6 Flight Trim -- 4.7 Flight Stability -- 4.8 Trim Drag -- 4.8.1 Minimum Drag -- 4.8.2 Relative Speed and Relative Drag -- 4.8.3 Variation of Minimum Drag Speed -- 4.8.4 Minimising 'Minimum' Drag -- 4.9 Steady-State Flight Performance -- 4.9.1 Definitions -- 4.9.2 Airspeeds for Maximum Endurance and Maximum Range -- 4.9.3 Range and Endurance -- 4.9.4 Alternative Form for Jet Aircraft Range and Endurance -- 4.9.5 Fuel Required to Carry Fuel.

4.10 Dynamic Modes -- Chapter 5 Gas Turbine Dynamics -- 5.1 Introduction -- 5.1.1 The Importance of Gas Turbines -- 5.1.2 What Chapter 5 Includes -- 5.1.3 What Chapter 5 Excludes -- 5.1.4 Overall Aim -- 5.2 Ideal Gas Properties -- 5.2.1 Equation of State -- 5.2.2 Energy, Enthalpy, and Entropy -- 5.2.3 Specific Heat Capacity -- 5.2.4 Adiabatic Gas Ratio -- 5.2.5 Compressible Gas Properties -- 5.2.6 Polytropic Processes -- 5.3 Gas Dynamics -- 5.3.1 Fundamental Relationships for Gas Flow -- 5.3.2 Speed of Sound -- 5.3.3 Bernoulli's Equation -- 5.3.4 Stagnation Conditions -- 5.4 Engine Components -- 5.4.1 Duct -- 5.4.2 Junction -- 5.4.3 Compressor -- 5.4.4 Split Compressor -- 5.4.5 Combustor -- 5.4.6 Turbine -- 5.4.7 Nozzle -- 5.5 Engine Dynamics -- 5.5.1 Shaft Speed Variation -- 5.5.2 Massflow Variation -- 5.5.3 Pressure Variation at Constant Temperature -- 5.5.4 Pressure and Temperature Variation -- 5.6 Engine Models -- 5.6.1 Turbojet Engine -- 5.6.1.1 Turbojet Specification -- 5.6.1.2 Turbojet Initialisation -- 5.6.1.3 Turbojet Physics -- 5.6.1.4 Turbojet Dynamics -- 5.6.2 Turbofan Engine -- 5.7 Gas Properties Data -- 5.7.1 Summary of Gas Properties -- 5.7.2 Gas Mixtures defined by Mass Fractions -- 5.7.3 Gas Mixtures defined by Mole Fractions -- 5.7.4 Dry Air -- 5.7.5 Fuel/Air Combustion Products -- Chapter 6 Additional Topics -- 6.1 Introduction -- 6.1.1 Expanding the Scope of Volume 2 -- 6.1.2 What Chapter 6 Includes -- 6.1.3 What Chapter 6 Excludes -- 6.1.4 Overall Aim -- 6.2 Structural Models -- 6.2.1 Equations of Motion -- 6.2.2 Coordinate Transformations -- 6.2.3 Coupled Structure -- 6.2.4 Wing-Fuselage Structure -- 6.2.5 Whole Aircraft Structure -- 6.3 Mass Distribution -- 6.3.1 Mass Properties -- 6.3.2 Transforming Mass Properties -- 6.3.3 Combining Mass Properties -- 6.3.4 Fuel Mass Distribution -- Bibliography -- Index -- EULA.