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Performance, Stability, Dynamics and Control of Airplanes

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ISBN-10: 1563475839

ISBN-13: 9781563475832

Edition: 2nd 2003

Authors: Bandu N. Pamadi

List price: $119.95
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Book details

List price: $119.95
Edition: 2nd
Copyright year: 2003
Publisher: American Institute of Aeronautics & Astronautics
Publication date: 1/31/2004
Binding: Hardcover
Pages: 768
Size: 6.50" wide x 9.50" long x 1.75" tall
Weight: 3.146
Language: English

Preface
Preface to the Previous Edition
Review of Basic Aerodynamic Principles
Introduction
Fluid Flow over Wings and Bodies
Drag of Bodies
Wing Parameters
Aerodynamic Characteristics of Wing Sections
Aerodynamic Characteristics of Finite Wings
Methods of Reducing Induced Drag
Tip Vortices: Formation and Hazards
Flow of a Compressible Fluid
Aerodynamic Forces in Supersonic Flow
Critical Mach Number
Area Rule
Summary
References
Problems
Aircraft Performance
Introduction
Equations of Motion for Flight in Vertical Plane
Gliding Flight
Level Flight
Climbing Flight
Range and Endurance
Endurance
Turning Flight
Takeoff and Landing
Hazards During Takeoff and Landing: Windshear and Microburst
Summary
References
Problems
Static Stability and Control
Introduction
Concept of Equilibrium and Stability
Static Longitudinal Stability
Stability in Maneuvering Flights
Static Directional Stability
Lateral Stability
Summary
References
Problems
Equations of Motion and Estimation of Stability Derivatives
Introduction
Axes Systems
Equations of Motion and Concept of Moving Axes System
Estimation of Stability Derivatives
Summary
References
Problems
Linear Systems, Theory, and Design: A Brief Review
Introduction
Laplace Transform
Transfer Function
System Response
Steady-State Errors of Unity Feedback Systems
Frequency Response
Stability of Closed-Loop Systems
Relations Between Time-Domain and Frequency-Domain Parameters
Design of Compensators
State-Space Analysis and Design
Summary
References
Problems
Airplane Response and Closed-Loop Control
Introduction
Longitudinal Response
Lateral-Directional Response
Flying Qualities
Closed-Loop Flight Control
Summary
References
Problems
Inertia Coupling and Spin
Introduction
Inertia Coupling
Autorotation of Wings and Fuselages
Airplane Spin
Equations of Motion for Steady-State Spin
Spin Recovery
Geometrical Modifications to Improve Spin Resistance
Summary
References
Problems
Stability and Control Problems at High Angles of Attack
Introduction
A Brief Historical Sketch
Brief Overview of High-Alpha Problems
Delta Wings at High Angles of Attack
Leading-Edge Extensions
Forebodies at High Angles of Attack
Relation Between Angle of Attack, Sideslip, and Roll Angle
Wing Rock
Roll Attractor of Delta Wings
Forebody-Induced Wing Rock
Suppression of Wing Rock
Roll Reversal and Yaw Departure
Control Concepts at High Angles of Attack
Summary
References
Standard Atmospheres
Table of Laplace Transforms
Cramer's Rule
Conversion of U.S. Customary Units to SI Units
Solved Examples
Bibliography
Index
Series Listing