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Beschreibung
"Flight Dynamics, first published in 2004, took a new approach to the science and mathematics of aircraft flight, unifying principles of aeronautics with contemporary systems analysis. While presenting traditional material that is critical to understanding aircraft motions, it does so in the context of modern computational tools and multivariable methods. Robert Stengel devotes particular attention to models and techniques that are appropriate for analysis, simulation, evaluation of flying qualities, and control system design. He establishes bridges to classical analysis and results, and explores new territory that was treated only inferentially in earlier books. The second edition will provide updates that cover new developments in aviation. Substantive changes include the addition of examples that relate to contemporary aircraft types, such as uninhabited air vehicles (UAVs), electrically powered airplanes, blended wing-body configurations, supersonic and hypersonic cruisers, and sub-orbital aerospace planes"--
"Flight Dynamics, first published in 2004, took a new approach to the science and mathematics of aircraft flight, unifying principles of aeronautics with contemporary systems analysis. While presenting traditional material that is critical to understanding aircraft motions, it does so in the context of modern computational tools and multivariable methods. Robert Stengel devotes particular attention to models and techniques that are appropriate for analysis, simulation, evaluation of flying qualities, and control system design. He establishes bridges to classical analysis and results, and explores new territory that was treated only inferentially in earlier books. The second edition will provide updates that cover new developments in aviation. Substantive changes include the addition of examples that relate to contemporary aircraft types, such as uninhabited air vehicles (UAVs), electrically powered airplanes, blended wing-body configurations, supersonic and hypersonic cruisers, and sub-orbital aerospace planes"--
Über den Autor
Robert F. Stengel
Inhaltsverzeichnis
- Preface to the Second Edition
- Chapter 1 Introduction
- 1.1 ELEMENTS OF THE AIRPLANE
- Airframe Components
- Propulsion Systems
- 1.2 REPRESENTATIVE AIRCRAFT
- Light General Aviation Aircraft
- Uninhabited Air Vehicle
- Variable-Stability Research Aircraft
- Sailplane
- Business Jet Aircraft
- Turboprop Commuter Aircraft
- Small Jet Transport Aircraft
- Medium Jet Transport Aircraft
- Large Jet Transport Aircraft
- Fighter/Attack Aircraft
- Jet Trainer Aircraft
- Hybrid Wing Body Aircraft
- Supersonic and Hypersonic Transport Aircraft
- Lifting Reentry Spacecraft
- 1.3 THE MECHANICS OF FLIGHT
- Text Box: Scalars, Vectors, and Matrices
- Text Box: Derivatives and Integrals of Time-Dependent Variables
- 1.4 COURSES IN FLIGHT DYNAMICS
- REFERENCES FOR CHAPTER 1
- Chapter 2 Exploring the Flight Envelope
- Text Box: Newton’s Laws of Motion
- 2.1 THE EARTH’S ATMOSPHERE
- Pressure, Density, and the Speed of Sound
- Viscosity, Humidity, and Rain
- Wind Fields and Atmospheric Turbulence
- 2.2 KINEMATIC EQUATIONS
- Translational Position and Velocity
- Angular Orientation and Rate
- Text Box: Matrix Inverse
- Airflow Angles
- Summary of Axis Systems and Transformations
- 2.3 FORCES AND MOMENTS
- Alternative Axis Systems
- Aerodynamic Forces and Moments
- 2.4 STATIC AERODYNAMIC COEFFICIENTS
- Lift
- Drag
- Pitching Moment
- Side Force
- Yawing Moment
- Rolling Moment
- Ground Effect
- 2.5 AIRCRAFT PROPULSION
- Power and Thrust
- Propulsion Systems
- Propellers and Ducted Fans
- Reciprocating Engines
- Turboprop, Turbofan, and Turbojet Engines
- Ramjet and Scramjet Engines
- Electric Powerplants
- General Thrust Models
- 2.6 FLIGHT PERFORMANCE
- Straight-and-Level Flight
- Steady Flight Envelope
- Cruising Range
- Gliding Flight
- Climbing Flight
- Maneuvering Envelope
- Steady Turning Flight
- Text Box: Performance of the North American P-51D Mustang
- REFERENCES FOR CHAPTER 2
- Chapter 3 The Dynamics of Aircraft Motion
- 3.1 MOMENTUM AND ENERGY
- Translational Momentum, Work, Energy, and Power
- Energy Height and Specific Excess Power
- Energy-Changing Maneuvers
- Angular Momentum and Energy
- 3.2 DYNAMIC EQUATIONS FOR A FLAT EARTH
- Rigid-Body Dynamic Equations
- Scalar Equations for a Symmetric Aircraft
- Avoiding the Euler Angle Propagation Singularity
- Direction Cosine Matrix
- Quaternion
- Alternative Reference Frames
- Air-Mass-Relative Reference Frame
- Alternative Body Frame
- Principal Axis Frame
- Text Box: Eigenvalues and Eigenvectors
- Stability Axes
- Acceleration Sensed at an Arbitrary Point
- 3.3 DYNAMIC EQUATIONS FOR A ROUND, ROTATING EARTH
- Geometry and Gravity Field of the Earth
- Rigid-Body Dynamic Equations for a Spherical Earth
- 3.4 AERODYNAMIC EFFECTS OF ROTATIONAL AND UNSTEADY MOTION
- Pitch-Rate Effects
- Angle-of-Attack-Rate Effects
- Yaw-Rate Effects
- Roll-Rate Effects
- Effects of Wind Shear and Wake Vortices
- 3.5 AERODYNAMIC EFFECTS OF CONTROL
- Trailing-Edge Flaps
- Wing-Mounted Control Surfaces
- Elevators, Stabilators, Elevons, and Canards
- Rudder
- Ailerons
- Other Control Devices
- Isolated Control Surfaces at High Deflection Angle and Angle of Attack
- 3.6 SOLUTION OF NONLINEAR DIFFERENTIAL EQUATIONS
- Numerical Algorithms for Integration
- Equations of Motion
- Continuous Representation of Tabulated Data
- Scalar Polynomials
- Multivariate Polynomials
- Computational Neural Networks
- Trimmed Solution of the Equations of Motion
- REFERENCES FOR CHAPTER 3
- Chapter 4 Methods of Analysis and Design
- 4.1 LOCAL LINEARIZATION OF DIFFERENTIAL EQUATIONS
- Stability-and-Control Derivatives
- Incorporating Unsteady Aerodynamic Effects
- Symmetric Aircraft in Wings-Level Flight
- Longitudinal Equations of Motion
- Lateral-Directional Equations of Motion
- Stability-Axis Equations of Motion
- 4.2 SOLUTION OF LINEAR DIFFERENTIAL EQUATIONS
- Numerical Integration and State Transition
- Text Box: Superposition of Linear, Time-Invariant Dynamic Responses
- Static and Quasistatic Equilibrium Response to Inputs
- Initial Response to Control Inputs
- Controllability and Observability of Motions
- Truncation and Residualization
- 4.3 STABILITY AND MODES OF MOTION
- Stability of Transient Response
- Fourier and Laplace Transforms
- Modes of Aircraft Motion
- Phase Plane
- 4.4 FREQUENCY-DOMAIN ANALYSIS
- Transfer Functions and Frequency Response
- Bode Plot
- Text Box: Bode Plot of an Isolated Zero
- Nyquist Plot and Nichols Chart
- Root Locus
- 4.5 DEALING WITH UNCERTAINTY
- Random Variables and Processes
- Text Box: Stationary and Nonstationary Probability Density Functions
- Dynamic Response to Random Inputs and Initial Conditions
- Effects of System Parameter Variations
- System Survey
- Monte Carlo Evaluation
- Stochastic Root Locus
- 4.6 LINEAR AEROELASTICITY
- Stress, Strain, and Material Properties
- Monocoque and Semi-Monocoque Structures
- Force and Moments on a Simple Beam
- Static Deflection of a Simple Beam under Load
- Vibrations of a Simple Beam
- Bending Vibrations of a Uniform Beam
- Torsional Vibrations of a Uniform Beam
- Coupled Vibrations of an Elastically Restrained Rigid Airfoil
- Vibrations of a Complex Structure
- The Four-Block Model
- Fuel Slosh
- 4.7 PILOTING ACTIONS AND AIRCRAFT FLYING QUALITIES
- Modeling the Pilot
- Flying Qualities Criteria
- Levels of Autonomy
- REFERENCES FOR CHAPTER 4
- Chapter 5 Longitudinal Motions
- 5.1 LONGITUDINAL EQUATIONS OF MOTION
- 5.2 REDUCED-ORDER MODELS OF LONG-PERIOD MODES
- Second-Order Phugoid-Mode Approximation
- Equilibrium Response to Control and Disturbance
- Controllability and Observability
- Eigenvalues, Natural Frequency, and Damping Ratio
- Eigenvectors
- Root Locus Analysis of Parameter Variations
- Frequency Response
- Root Locus Analysis of Feedback Control
- Time Response
- Effects of Compressibility
- Effects of Altitude Variation
- Air Density, Sound Speed, and Gravity Variations
- Ground Effect
- Effects of Wind Shear
- 5.3 REDUCED-ORDER MODEL OF THE SHORT-PERIOD MODE
- Second-Order Approximation
- Equilibrium Response to Control and Disturbance
- Controllability and Observability
- Eigenvalues, Natural Frequency, and Damping Ratio
- Eigenvectors
- Root Locus Analysis of Parameter Variations
- Frequency Response
- Root Locus Analysis of Feedback Control
- Time Response
- Effects of Compressibility and High Angle of Attack
- 5.4 COUPLED PHUGOID/SHORT-PERIOD DYNAMICS
- Residualized Phugoid Mode
- Fourth-Order Model
- Equilibrium Response to Control
- Eigenvalues and Root Locus Analysis of Parameter Variations
- Transfer Functions and Frequency Response
- Response to Disturbances
- Root Locus Analysis of Feedback Control
- Time Response
- Longitudinal Flying Qualities
- 5.5 CONTROL MECHANISMS, STICK-FREE STABILITY, AND TRIM
- Elevator Control Mechanism
- Short-Period/Control-Mechanism Coupling
- Control Force for Trimmed Flight
- Elevator Angle and Stick Force per g
- “Tail-Wags-Dog” Effect
- 5.6 LONGITUDINAL AEROELASTIC EFFECTS
- Truncated and Residualized Aeroelastic Models
- Coupling of the Short Period with a Single Elastic Mode
- Equilibrium Response to Control
- Eigenvalues and Root Locus Evaluation of Parameter Variations
- Control and Disturbance Transfer Functions
- Frequency Response and the Effects of Feedback Control
- Effects of Elasticity on Time Response
- REFERENCES FOR CHAPTER 5
- Chapter 6 Lateral-Directional Motions
- 6.1 LATERAL-DIRECTIONAL EQUATIONS OF MOTION
- 6.2 REDUCED-ORDER MODEL OF THE DUTCH ROLL MODE
- Equilbrium Response to Control and Disturbance
- Controllability and Observability
- Eigenvalues, Natrual Frequency, and Damping Ratio
- Eigenvectors
- Root Locus Analysis of Parameter Variations
- Frequency Response
- Root Locus Analysis of Feedback Control
- Time Response
- 6.3 REDUCED-ORDER MODEL OF ROLL AND SPIRAL MODES
- Equilbrium Response to Control and Disturbance
- Controllability and Observability
- Eigenvalues, Natural Frequency, and Damping Ratio
- Eigenvectors
- Root Locus Analysis of Parameter Variations
- Frequency Response
- Root Locus Analysis of Feedback Control
- Time Response
- 6.4 COUPLED LATERAL-DIRECTIONAL DYNAMICS
- A Truncated Dutch Roll/Roll Model
- Residualized Lateral-Directional Models
- Residualized Dutch Roll...
- Second-Order Approximation
- Second-Order Phugoid-Mode Approximation
- 4.1 LOCAL LINEARIZATION OF DIFFERENTIAL EQUATIONS
- 3.1 MOMENTUM AND ENERGY
- 2.1 THE EARTH’S ATMOSPHERE
- 1.1 ELEMENTS OF THE AIRPLANE
Details
| Erscheinungsjahr: | 2022 |
|---|---|
| Fachbereich: | Mechanik & Akustik |
| Genre: | Importe, Physik |
| Rubrik: | Naturwissenschaften & Technik |
| Medium: | Buch |
| Inhalt: | Einband - fest (Hardcover) |
| ISBN-13: | 9780691220253 |
| ISBN-10: | 0691220255 |
| Sprache: | Englisch |
| Einband: | Gebunden |
| Autor: | Stengel, Robert F. |
| Hersteller: | Princeton University Press |
| Verantwortliche Person für die EU: | Libri GmbH, Europaallee 1, D-36244 Bad Hersfeld, gpsr@libri.de |
| Maße: | 261 x 185 x 53 mm |
| Von/Mit: | Robert F. Stengel |
| Erscheinungsdatum: | 01.11.2022 |
| Gewicht: | 1,838 kg |