INDICE: 1. Aircraft Equations of Motion 1.1 Introduction 1.2 Reference Frames and Assumptions 1.3 Conservation of the Linear Momentum Equations (CLMEs) 1.4 Conservation of the Angular Momentum Equations (CAMEs) 1.5 Conservation of the Angular Momentum Equations (CAMEs) with Rotor Effects 1.6 Euler Angles 1.7Flight Path Equations (FPEs) 1.8 Kinematic Equations (KEs) 1.9 Gravity Equations (GEs) 1.10 Summary of the Aircraft Equations of Motion 1.11 Definition of Steady-State and Perturbation Conditions 1.12 Aircraft Equations of Motion at Steady-State Conditions 1.13 Aircraft Equations of Motion at Perturbed Conditions 1.14 Small Perturbation Equations from a Steady-State Level Flight 1.15 Summary References Student Sample Problems Problems 2. Review of Basic Concepts of Aerodynamic Modeling 2.1 Introduction 2.2 Review of Key Aerodynamic Characteristics for Wing Sections 2.3 Wing Planforms and Wing Lift Curve Slope 2.4 Review of the Downwash Effect and Effectiveness of Control Surfaces 2.5 Determination of the Aerodynamic Center for Wing and Wing1Fuselage 2.6 Approaches to the Modeling of Aerodynamic Forces and Moments 2.7 Summary References Student Sample Problems Problems 3. Modeling of Longitudinal Aerodynamic Forces and Moments 3.1 Introduction 3.2 Aircraft Stability Axes 3.3 Modeling of the Longitudinal Steady-State Aerodynamic Forces and Moment 3.4 Modeling of FAX1 3.5 Modeling of FAZ1 3.6 Modeling of MA1 3.7 Aircraft Aerodynamic Center 3.8 Summary ofthe Longitudinal Steady-State Aerodynamic Forces and Moment 3.9 Modeling of the Longitudinal Small Perturbation Aerodynamic Forces and Moments 3.10 Summaryof Longitudinal Stability and Control Derivatives 3.11 Summary References Student Sample Problems Case Study Short Problems Problems 4. Modeling of LateralDirectional Aerodynamic Forces and Moments 4.1 Introduction 4.2 Modeling of FAY1 4.3 Modeling of LA1 4.4 Modeling of NA1 4.5 Summary of the Lateral Directional Steady-State Force and Moments 4.6 Modeling of the Small Perturbation Lateral Directional Aerodynamic Force and Moments 4.7 Summary of Longitudinal andLateral Directional Aerodynamic Stability and Control Derivatives 4.8 Final Overview and Ranking of the Importance of the Aerodynamic Coefficients 4.9 Summary of the Modeling of the Longitudinal and Lateral-Directional Aerodynamic Forces and Moments References Student Sample Problems Case Study Short Problems Problems 5. Review of Basic Aircraft Performance and Modeling of Thrust Forcesand Moments 5.1 Introduction 5.2 Review of Different Aircraft Propulsion Systems 5.3 Review of Basic Aircraft Performance 5.4 Power at Level Flight 5.5 Determination of Power Required 5.6 Determination of Power Available 5.7 Modelingof the Thrust Forces and Moments 5.8 Summary References Student Sample Problems Problems 6. Aircraft Stability and Design for Trim Conditions 6.1 Introduction 6.2 Concept of Aircraft Stability 6.3 Criteria for Aircraft Static Stability 6.4 Longitudinal Analysis of Steady-State St
- ISBN: 978-0-470-62667-2
- Editorial: John Wiley & Sons
- Encuadernacion: Cartoné
- Páginas: 832
- Fecha Publicación: 27/10/2011
- Nº Volúmenes: 1
- Idioma: Inglés