Buch, Englisch, 752 Seiten, Format (B × H): 164 mm x 240 mm, Gewicht: 1336 g
ISBN: 978-0-691-11407-1
Verlag: Princeton University Press
Flight Dynamics takes 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. This book combines a highly accessible style of presentation with contents that will appeal to graduate students and to professionals already familiar with basic flight dynamics.Dynamic analysis has changed dramatically in recent decades, with the introduction of powerful personal computers and scientific programming languages. Analysis programs have become so pervasive that it can be assumed that all students and practicing engineers working on aircraft flight dynamics have access to them. Therefore, this book presents the principles, derivations, and equations of flight dynamics with frequent reference to MATLAB functions and examples.By using common notation and not assuming a strong background in aeronautics, Flight Dynamics will engage a wide variety of readers. Introductions to aerodynamics, propulsion, structures, flying qualities, flight control, and the atmospheric and gravitational environment accompany the development of the aircraft's dynamic equations.
Autoren/Hrsg.
Fachgebiete
- Wirtschaftswissenschaften Wirtschaftssektoren & Branchen Fertigungsindustrie Luftfahrtindustrie
- Technische Wissenschaften Maschinenbau | Werkstoffkunde Technische Mechanik | Werkstoffkunde Strömungslehre
- Technische Wissenschaften Verkehrstechnik | Transportgewerbe Luft- und Raumfahrttechnik, Luftverkehr
- Technische Wissenschaften Technik Allgemein Mathematik für Ingenieure
- Naturwissenschaften Physik Mechanik Kontinuumsmechanik, Strömungslehre
Weitere Infos & Material
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 Freque
