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Preface | xv | |
Preface to the Previous Edition | xvii | |
Chapter 1. | Review of Basic Aerodynamic Principles | 1 |
1.1 | Introduction | 1 |
1.2 | Fluid Flow over Wings and Bodies | 2 |
1.3 | Drag of Bodies | 11 |
1.4 | Wing Parameters | 12 |
1.5 | Aerodynamic Characteristics of Wing Sections | 18 |
1.6 | Aerodynamic Characteristics of Finite Wings | 27 |
1.7 | Methods of Reducing Induced Drag | 31 |
1.8 | Tip Vortices: Formation and Hazards | 32 |
1.9 | Flow of a Compressible Fluid | 35 |
1.10 | Aerodynamic Forces in Supersonic Flow | 36 |
1.11 | Critical Mach Number | 40 |
1.12 | Area Rule | 59 |
1.13 | Summary | 64 |
References | 65 | |
Problems | 66 | |
Chapter 2. | Aircraft Performance | 67 |
2.1 | Introduction | 67 |
2.2 | Equations of Motion for Flight in Vertical Plane | 70 |
2.3 | Gliding Flight | 73 |
2.4 | Level Flight | 81 |
2.5 | Climbing Flight | 94 |
2.6 | Range and Endurance | 106 |
2.7 | Endurance | 114 |
2.8 | Turning Flight | 122 |
2.9 | Takeoff and Landing | 146 |
2.10 | Hazards During Takeoff and Landing: Windshear and Microburst | 156 |
2.11 | Summary | 158 |
References | 158 | |
Problems | 159 | |
Chapter 3. | Static Stability and Control | 165 |
3.1 | Introduction | 165 |
3.2 | Concept of Equilibrium and Stability | 165 |
3.3 | Static Longitudinal Stability | 168 |
3.4 | Stability in Maneuvering Flights | 249 |
3.5 | Static Directional Stability | 259 |
3.6 | Lateral Stability | 294 |
3.7 | Summary | 313 |
References | 313 | |
Problems | 314 | |
Chapter 4. | Equations of Motion and Estimation of Stability Derivatives | 321 |
4.1 | Introduction | 321 |
4.2 | Axes Systems | 322 |
4.3 | Equations of Motion and Concept of Moving Axes System | 361 |
4.4 | Estimation of Stability Derivatives | 391 |
4.5 | Summary | 438 |
References | 439 | |
Problems | 440 | |
Chapter 5. | Linear Systems, Theory, and Design: A Brief Review | 443 |
5.1 | Introduction | 443 |
5.2 | Laplace Transform | 444 |
5.3 | Transfer Function | 449 |
5.4 | System Response | 450 |
5.5 | Steady-State Errors of Unity Feedback Systems | 457 |
5.6 | Frequency Response | 460 |
5.7 | Stability of Closed-Loop Systems | 464 |
5.8 | Relations Between Time-Domain and Frequency-Domain Parameters | 488 |
5.9 | Design of Compensators | 491 |
5.10 | State-Space Analysis and Design | 510 |
5.11 | Summary | 536 |
References | 536 | |
Problems | 536 | |
Chapter 6. | Airplane Response and Closed-Loop Control | 541 |
6.1 | Introduction | 541 |
6.2 | Longitudinal Response | 541 |
6.3 | Lateral-Directional Response | 569 |
6.4 | Flying Qualities | 595 |
6.5 | Closed-Loop Flight Control | 599 |
6.6 | Summary | 626 |
References | 627 | |
Problems | 627 | |
Chapter 7. | Inertia Coupling and Spin | 631 |
7.1 | Introduction | 631 |
7.2 | Inertia Coupling | 631 |
7.3 | Autorotation of Wings and Fuselages | 644 |
7.4 | Airplane Spin | 650 |
7.5 | Equations of Motion for Steady-State Spin | 653 |
7.6 | Spin Recovery | 667 |
7.7 | Geometrical Modifications to Improve Spin Resistance | 668 |
7.8 | Summary | 674 |
References | 675 | |
Problems | 676 | |
Chapter 8. | Stability and Control Problems at High Angles of Attack | 677 |
8.1 | Introduction | 677 |
8.2 | A Brief Historical Sketch | 677 |
8.3 | Brief Overview of High-Alpha Problems | 678 |
8.4 | Delta Wings at High Angles of Attack | 680 |
8.5 | Leading-Edge Extensions | 690 |
8.6 | Forebodies at High Angles of Attack | 694 |
8.7 | Relation Between Angle of Attack, Sideslip, and Roll Angle | 699 |
8.8 | Wing Rock | 699 |
8.9 | Roll Attractor of Delta Wings | 714 |
8.10 | Forebody-Induced Wing Rock | 718 |
8.11 | Suppression of Wing Rock | 729 |
8.12 | Roll Reversal and Yaw Departure | 736 |
8.13 | Control Concepts at High Angles of Attack | 739 |
8.14 | Summary | 753 |
References | 754 | |
Appendix A. | Standard Atmospheres | 757 |
Appendix B. | Table of Laplace Transforms | 761 |
Appendix C. | Cramer's Rule | 763 |
Appendix D. | Conversion of U.S. Customary Units to SI Units | 765 |
Appendix E. | Solved Examples | 767 |
Bibliography | 769 | |
Index | 771 | |
Series Listing | 781 |
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Add Performance, Stability, Dynamics, and Control of Airplanes, Second Edition, This book provides a comprehensive and integrated exposure to airplane performance, stability, dynamics, and flight control. The text supports a two-semester course for senior undergraduate or first-year graduate students in aerospace engineering. Basic a, Performance, Stability, Dynamics, and Control of Airplanes, Second Edition to the inventory that you are selling on WonderClubX
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Add Performance, Stability, Dynamics, and Control of Airplanes, Second Edition, This book provides a comprehensive and integrated exposure to airplane performance, stability, dynamics, and flight control. The text supports a two-semester course for senior undergraduate or first-year graduate students in aerospace engineering. Basic a, Performance, Stability, Dynamics, and Control of Airplanes, Second Edition to your collection on WonderClub |