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Produktbild: Flight Dynamics

Flight Dynamics

142,99 €

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Beschreibung

Produktdetails

Einband

Gebundene Ausgabe

Erscheinungsdatum

17.10.2004

Verlag

Princeton University Press

Seitenzahl

864

Maße (L/B/H)

24/16,4/4,7 cm

Gewicht

1336 g

Sprache

Englisch

ISBN

978-0-691-11407-1

Beschreibung

Produktdetails

Einband

Gebundene Ausgabe

Erscheinungsdatum

17.10.2004

Verlag

Princeton University Press

Seitenzahl

864

Maße (L/B/H)

24/16,4/4,7 cm

Gewicht

1336 g

Sprache

Englisch

ISBN

978-0-691-11407-1

Herstelleradresse

Libri GmbH
Europaallee 1
36244 Bad Hersfeld
DE

Email: gpsr@libri.de

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  • Produktbild: Flight Dynamics
  • Preface 1. Introduction Elements of the Airplane Airframe Components Propulsion Systems Representative Flight Vehicles Light General Aviation Aircraft Variable-Stability Research Aircraft Sailplane Business Jet Aircraft Turboprop Commuter Aircraft Small Commercial Transport Aircraft Large Commercial Transport Aircraft Supersonic Transport Aircraft Fighter/Attack Aircraft Bomber Aircraft Space Shuttle Uninhabited Air Vehicle The Mechanics of Flight References for Chapter 1 2. Exploring the Flight Envelope The Earth's Atmosphere Pressure, Density, and the Speed of Sound Viscosity, Humidity, and Rain Wind Fields and Atmospheric Turbulence Kinematic Equations Translational Position and Velocity Angular Orientation and Rate Airflow Angles Summary of Axis Systems and Transformations Forces and Moments Alternative Axis Systems Aerodynamic Forces and Moments Static Aerodynamic Coefficients Lift Drag Pitching Moment Side Force Yawing Moment Rolling Moment Ground Effect Thrusting Characteristics of Aircraft Powerplants Propellers Reciprocating Engines Turboprop, Turbofan, and Turbojet Engines Ramjet and Scramjet Engines Steady Flight Performance Straight-and-Level Flight Steady Flight Envelope Cruising Range Gliding Flight Climbing Flight Maneuvering Envelope Steady Turning Flight References for Chapter 2 3. The Dynamics of Aircraft Motion Momentum and Energy Translational Momentum, Work, Energy, and Power Energy-Changing Maneuvers Angular Momentum and Energy Dynamic Equations for a Flat Earth Rigid-Body Dynamic Equations Scalar Equations for a Symmetric Aircraft Alternative Frames of Reference Inertial Reference Frames Body-Axis Reference Frames Velocity- and Wind-Axis Reference Frames Air-Mass-Relative Reference Frame Direction Cosines and Quaternions Acceleration Sensed at an Arbitrary Point Dynamic Equations for a Round, Rotating Earth Geometry and Gravity Field of the Earth Rigid-Body Dynamic Equations 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 Aerodynamic Effects of Control Elevators, Stabilators, Elevons, and Canards Rudders Ailerons Spoilers and Flaps Other Control Devices Isolated Control Surfaces Trailing-Edge Flaps Solution of Nonlinear Differential Equations Numerical Algorithms for Integration Equations of Motion Representation of Data Trimmed Solution of the Equations of Motion References for Chapter 3 4. Methods of Analysis and Design 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 Solution of Linear Differential Equations Numerical Integration and State Transition Static and Quasistatic Equilibrium Response to Inputs Initial Response to Control Inputs Controllability and Observability of Motions Truncation and Residualization Stability and Modes of Motion Stability of Transient Response Fourier and Laplace Transforms Modes of Aircraft Motion Phase Plane Frequency-Domain Analysis Transfer Functions and Frequency Response Nyquist Plot and Nichols Chart Root Locus Dealing with Uncertainty Random Variables and Processes Dynamic Response to Random Inputs and Initial Conditions Effects of System Parameter Variations System Survey Monte Carlo Evaluation Stochastic Root Locus 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 Coupled Vibrations of an Elastically Restrained Rigid Airfoil Vibrations of a Complex Structure The Four-Block Structure Fuel Slosh Introduction to Flying Qualities and Flight Control Systems Cognitive/Biological Models and Piloting Action Aircraft Flying Qualities Linear-Quadratic Regulator Steady-State Response to Command Input Implicit Model-Following and Integral Compensation Optimal State Estimation Linear-Quadratic-Gaussian Regulator Design for Stochastic Robustness References for Chapter 4 5. Longitudinal Motions Longitudinal Equations of Motion Reduced-Order Models of Long-Period Modes Second-Order Phugoid-Mode Approximation Effects of Compressibility Effects of Altitude Variation Effects of Wind Shear Reduced-Order Model of the Short-Period Mode Second-Order Approximation Effects of Compressibility and High Angle of Attack Coupled Phugoid/Short-Period Dynamics Residualized Phugoid Mode Fourth-Order Model Longitudinal Flying Qualities 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 Longitudinal Aeroelastic Effects Truncated and Residualized Elastic-Body Models Coupling of the Short Period with a Single Elastic Mode References for Chapter 5 6. Lateral-Directional Motions Lateral-Directional Equations of Motion Reduced-order Model of the Dutch Roll Mode Reduced-order Model of Roll and Spiral Modes Coupled Lateral-Directional Dynamics A Truncated Dutch roll/Roll Model Residualized Lateral-Directional Models Fourth-Order Model Lateral-Directional Flying Qualities Control Mechanisms, Nonlinearity, and Time Delay Rudder Control Mechanism Dutch roll/Rudder Coupling Quasi-linear Representation of Nonlinearity Quasi-linear Root Locus Analysis Roll-Spiral/Aileron Coupling Spoiler Nonlinearity and Time Delay Lateral-Directional Aeroelastic Effects Equilibrium Response to Control Eigenvalues and Root Locus Analysis of Parameter Variations Response to Initial Conditions and Step Control Inputs References for Chapter 6 7. Coupled Longitudinal and Lateral-Directional Motions Small-amplitude Motions Effects of Rotating Machinery Asymmetric Inertial and Aerodynamic Properties Asymmetric Flight Condition and Constant Angular Rate Coupling Controls Inertial Coupling of Pitch and Yaw Motions Fifth-Order Model of Coupled Dynamics Truncated and Residualized Fourth-Order Models Response to Controls During Steady Rolling Multiple Equilibrium Points Second-order Examples of Multiple Equilibria Effects of Cross-Coupling and Control on Rolling Equilibrium Flight at High Angle of Attack High-Angle-of-Attack Aerodynamics and Control Effects Fully Developed Spins Simulated Motions of a Business Jet Aircraft Stability of High-Angle-of-Attack Maneuvers Pilot-Aircraft Interactions Gain-Scheduled Stability and Command Augmentation Adaptive Neural Network Control Robust Nonlinear-Inverse-Dynamic Control References for Chapter 7 Epilogue Appendices Constants, Units, and Conversion Factors Mathematical Model and Six-Degree-of-Freedom Simulation of a Business Jet Aircraft Main Program for Analysis and Simulation (FLIGHT) Low-Angle-of-Attack, Mach-Dependent Model (LoAeroModel) High-Angle-of-Attack, Low-Subsonic Model (HiAeroModel) Supporting Functions Equations of Motion (EoM) Cost Function for Aerodynamic Trim (TrimCost) Direction Cosine Matrix (DCM) Linear System Matrices (LinModel) Wind Field (WindField) Atmospheric State (Atmos) Linear System Survey Main Program for Analysis and Simulation (SURVEY) Supporting Functions Reduced-Order Models (LonLatDir) Transient Response (Trans) Static Response (Static) Controllability and Observability (ConObs) Natural Frequency (NatFreq) Stability and Modes of Motion (StabMode) Paper Airplane Program Bibliography of NASA Reports Related to Aircraft Configuration Aerodynamics