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Front Cover 1 Aircraft Dynamic Stability and Response 4 Copyright Page 5 Table of Contents 6 Preface 10 List Of Symbols 12 NON-DIMENSIONAL FORMS OF THE AERODYNAMIC DERIVATIVES USED IN AMERICA 22 UNITS 24 Part I: FLIGHT DYNAMICS 26 Chapter 1. INTRODUCTION 28 THE GENERAL MEANING OF STABILITY 28 LONGITUDINAL STATIC STABILITY 29 STATIC MARGIN 31 STABILITY AND TRIM 33 MANOEUVRABILITY AND MANOEUVRE MARGIN 34 REFERENCES 35 PROBLEMS 35 Chapter 2. THE EQUATIONS OF MOTION 38 INTRODUCTION 38 THE GENERAL DYNAMICAL EQUATIONS FOR A RIGID AIRCRAFT REFERRED TO MOVING AXES 38 DEFINITION OF THE ANGLE OF PITCH θ, THE ANGLE OF BANK Φ AND ANGLE OF YAW ψ 40 RELATIONS FOR RATES OF ROLL, PITCH AND YAW 41 DETERMINATION OF THE GRAVITATIONAL FORCES 42 ANGLES OF YAW AND SIDESLIP 43 DETERMINATION OF THE AERODYNAMIC FORCES 44 SEPARABILITY OF LONGITUDINAL AND LATERAL MOTION 46 AXIS SYSTEMS USED IN STABILITY ANALYSIS 47 NON-DIMENSIONAL AERODYNAMIC DERIVATIVES (LONGITUDINAL) 47 NON-DIMENSIONAL AERODYNAMIC DERIVATIVES (LATERAL) 49 NON-DIMENSIONAL DISTURBANCES 50 NON-DIMENSIONAL MASS AND INERTIA 51 NON-DIMENSIONAL FORM OF THE EQUATIONS OF MOTION 51 THE MOTION OF THE CENTRE OF GRAVITY OF THE AIRCRAFT 53 REFERENCES 54

Author

A. W. Babister M.A.,Ph.D.,M.R.Ae.S.

Publisher

Pergamon Press

Language

EN