Aircraft Lateral Dynamics Using a procedure similar to the longitudinal case, we can develop the equa tions of motion for the lateral dynamics

美国麻省理工大学：《Aerospace Dynamics（航空动力学）》英文版 Lecture 15

Spring 2003 Derivation of lagrangian equations Basic Concept: Virtual Work Consider system of N particles located at(, x2, x,,.x3N )with 3 forces per particle(f. f, f..fn). each in the positive direction

一、变化的可能性与现实性 可能的变化是否一定发生? 可能性大、自发趋势大的反应是否速率也快?

UPTO NoW HAVE CONJSI DERED PROBLEMS RELEVANT To THE RIGID BO0Y OYNAMICS THAT ARE IMPORTANT To AEROSPACE VEHICLES USED A BODy FRAME THAT ROTATES WITH THE VEHICLE ANOTHER TMPORTANT CLASS oF PRoBLEMS FoR Bo DIES SUCH AS GyRoscofes ROToR WITH HIGH SPIN RATE ESSENTIALY MASSLESS FRAME

Aircraft Lateral Dynamics Using a procedure similar to the longitudinal case, we can develop the equa tions of motion for the lateral dynamics

《工程科学学报》：微波场下的钒渣氯化动力学

东华大学：材料科学与工程实验教学资源（讲义）加聚反应动力学-膨胀法测反应速度

东华大学：材料科学与工程实验教学资源（讲义）光学解偏振法测定高聚物结晶动力学速度常数

东华大学：材料科学与工程实验教学资源（讲义）加聚反应动力学——膨胀计法测反应速度