Performance, Stability, Dynamics, and Control of Airplanes |
Contents
Introduction | 1 |
Aircraft Performance | 67 |
7 | 114 |
xii | 165 |
Equations of Motion and Estimation | 321 |
A Brief Review | 443 |
Airplane Response and ClosedLoop Control | 541 |
Inertia Coupling and Spin | 631 |
Stability and Control Problems at High Angles | 677 |
| 754 | |
Appendix B Table of Laplace Transforms | 761 |
Appendix E Solved Examples | 767 |
Static Stability and Control | |
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Common terms and phrases
aerodynamic center aileron aircraft airfoil altitude angle of attack angular velocity aspect ratio assume aviation airplane axis body axes system C₁ center of gravity closed-loop cosē damping deg/s delta wing dihedral directional stability disturbance dynamic effect elevator deflection equations estimation Euler angles exposed wing flight velocity forebody frequency fuselage given by Eq high angles horizontal tail inertial input lateral-directional leading edge leading-edge level flight lift coefficient lift-curve slope longitudinal Mach number matrix maximum method motion obtain parameter phugoid pitch pitching moment plane positive rad/s response Reynolds number roll root chord root-locus rudder Schematic shown in Fig side force sideslip spin stall steady-state stick force stick-free strip theory subsonic speeds supersonic speeds surface transfer function trim variation vertical tail wing contribution wing rock zero