History and Policy in the Fifties Reading: Chapters 1-10, The Heavens and the Earth Big Themes: Technocracy as a way for a nation to accomplish tasks mon The impact of the thermonuclear bomb and the technology of missiles The Cold War as a contest between Communism and Capitalism
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Space Policy Seminar#1 What is space policy? Who makes it and Why is it important? Outlineo Definitions Technical statement and limits A simple model for space policy statements
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一、起落架的载荷情况多 二、需要作机构运动 三、要从受力要求的观点和机构运动要求的观 点来分析起落架的构造
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结构刚度不足对飞机最主要的影响在于, 飞机在飞行速度范围内可能会发生气动弹 性现象,这时的刚度判据就是发生气动弹 性现象时的临界速度V,结构刚度必须要 满足条件V>Vm 气动弹性是与飞机上的气动力、惯性力和 结构的弹性力相关的,是由于飞机在飞行 时载荷作用下的变形和弹性引起的
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16.61 Aerospace Dynamics 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
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16.61 Aerospace Dynamics Spring 2003 Example Given: Catapult rotating at a constant rate(frictionless, in the horizontal plane) Find the eom of the particle as it leaves the
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16.61 Aerospace Dynamics Spring 2003 Lagrange's equations Joseph-Louis lagrange 1736-1813 http://www-groups.dcs.st-and.ac.uk/-history/mathematicians/lagranGe.html Born in Italy. later lived in berlin and paris Originally studied to be a lawyer
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NUMERICAL SoL°To ·G川EN舟c。 MPLEX SET of0 YNAMICS 义(t)=斤(x,x) WHERE f()CouL0BE升MNLE升 R FUNCTI0N 工TCNB.工 MOss8 LE To ACTVALLY SoLVE FoR×(t)∈ ACTLY →0 EVELoP A则 UMERICAL SOLUTION. cA小NE0co0 ES TO HELP v5 D。TwsτN MATLAB BUT LET US CONSIDER THE BAsIcs
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ECTURE +2 RIGId BoDY DYNAnIC 工Ap1CAT105FA。R工 GENERAL ROTATIONAL JYNMICS EULER'S EQuATIoN of MOTIoN TORQVE fREE SPECIAL CAsEs PRIMARY LESSONS 3D RoTATONAL MOTION MUCH MORE COMPLEX
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RIGI0 BoDY DYNAMICS ·T叭ocAP0 NENTS千0RtG1D80 y MoTIo 千 RANSLAT(0NAL F= M R升 TIONAL D ECOU PLE PRO vIED 工ND0FRTT0A AA0A工Nb0FTRA5L|N
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