Performance, Stability, Dynamics, and Control of AirplanesAmerican Institute of Aeronautics and Astronautic, 1998 - 766 sidor A textbook for a two-semester senior undergraduate or first-year graduate course in aerospace. Includes the necessary background material on basic aerodynamics, dynamics, and linear control. Assumes the airplane is a rigid body and therefore does not consider elastic deformations and their effects on an airplane's motion. Includes a number of solved examples to illustrate the theory and basic principles, and several exercise problems to help develop problem- solving skills. Annotation copyrighted by Book News, Inc., Portland, OR |
Innehåll
Aircraft Performance | 67 |
Static Stability and Control | 165 |
Equations of Motion and Estimation | 319 |
Upphovsrätt | |
6 andra avsnitt visas inte
Andra upplagor - Visa alla
Performance, Stability, Dynamics, and Control of Airplanes Bandu N. Pamadi Begränsad förhandsgranskning - 2004 |
Performance, Stability, Dynamics, and Control of Airplanes Bandu N. Pamadi Fragmentarisk förhandsgranskning - 2004 |
Vanliga ord och fraser
aerodynamic center aileron aircraft airfoil altitude angle of attack angular velocity approximately aspect ratio assume aviation airplane axes system axis C₁ center of gravity chord closed-loop damping ratio Datcom deflection deg/s delta wing directional stability drag coefficient dynamic effect elevator Euler angles feedback flight velocity flow separation forebody frequency fuselage given by Eq high angles horizontal tail induced drag inertia input lateral-directional leading edge leading-edge level flight lift coefficient lift-curve slope load factor longitudinal m₁ Mach number matrix maximum method motion Nyquist plot obtain parameter phase-variable form phugoid pitch pitching moment poles pressure rad/s response Reynolds number root chord root-locus rudder s-plane Schematic sections short-period shown in Fig side force sideslip spin stall static steady-state strake strip theory subsonic speeds supersonic speeds surface thrust transfer function variation vertical tail vortex breakdown wing rock zero
Hänvisningar till den här boken
Journal of Aerospace Sciences and Technologies: A Quarterly ..., Volym 55 Fragmentarisk förhandsgranskning - 2003 |