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Phase Change Heat Conduction in General Orthogonal Curvilinear Coordinates. 一般正交曲线坐标下的相变热传导。
Pub Date : 1979-02-01 DOI: 10.2514/6.1979-181
Leon Bledjian
Abstract : The approximate method of London and Seban for predicting the solidification rate and for melting in or around slabs, cylinders, and spheres has been reformulated in genral orthogonal curvilinear coordinates. Closed-form solutions are presented for the rate of phase change and temperature drop as a function of a nondimensional time, STeFo (product of Stefan and Fourier numbers), for various geometries including elliptic cylinders, spheroids of varying eccentricites, and bicylindrical problems. Both convection and flux boundary conditions which can vary with time are considered. The effect of Biot number on phase change times and the resulting boundary temperature are presented in graphical form for some of the geometries considered. The method's degree of approximation is investigated by comparison with published analytical results. The approximate applicability of the equations to some special phase change conduction problems is demostrated. (Author)
摘要:在一般正交曲线坐标下,重新制定了用于预测凝固速率和在板坯、圆柱体和球体内或周围熔化的伦敦和塞班近似方法。对于各种几何形状,包括椭圆圆柱体、不同偏心距的球体和双圆柱体问题,提出了相变速率和温度下降作为无因次时间的函数STeFo(斯特凡数和傅立叶数的乘积)的封闭形式的解决方案。考虑了随时间变化的对流和通量边界条件。对于所考虑的一些几何形状,Biot数对相变时间和边界温度的影响以图形形式给出。通过与已发表的分析结果的比较,研究了该方法的近似程度。对一些特殊的相变传导问题证明了方程的近似适用性。(作者)
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引用次数: 1
Communications in Orbit: A Legal Analysis and Prognosis 轨道通信:法律分析与预测
Pub Date : 1966-05-04 DOI: 10.1016/B978-1-4832-2716-0.50056-6
J. Morenoff
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引用次数: 0
Establishment and Maintenance of a Communication Satellite System 通信卫星系统的建立和维护
Pub Date : 1966-05-04 DOI: 10.1016/B978-1-4832-2716-0.50042-6
D. Werts
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引用次数: 0
Limiting orbits around the equilateral centers of libration 围绕等边振动中心的极限轨道
Pub Date : 1966-03-01 DOI: 10.1086/109859
A. Deprit
Publisher Summary This chapter describes the limiting orbits at the equilateral centers of libration. The planar restricted problem of three bodies is presented by the Hamiltonian function. For all these mass ratios, the limiting orbits have exhibited nontrivial characteristic exponents of the stable type. This result is somewhat puzzling. It has been suggested that the limiting orbits could perhaps be identified with that doubly asymptotic periodic orbit, which is the homoclinic solution common to the two manifolds of asymptotic solutions generated at the unstable equilibrium point. The fact that the limiting orbits have characteristic exponents of the stable type makes it embarrassing to accept this conjecture. Once the existence of limiting periodic orbits has been established, one can face the second part of Browns hypothesis. Each limiting orbit for a fixed value of the mass ratio μ should be the head of two families of periodic librations and for the first family, the period would decrease together with the Jacobi constant, whereas for the second family, the period would increase together with the Jacobi constant.
本章描述在等边中心的极限轨道。用哈密顿函数给出了三体的平面约束问题。对于所有这些质量比,极限轨道都表现出稳定型的非平凡特征指数。这个结果有些令人费解。在不稳定平衡点处生成的两个渐近解流形的同宿解表明,极限轨道可以用双渐近周期轨道来识别。极限轨道具有稳定型特征指数这一事实使我们难以接受这一猜想。一旦确定了有限周期轨道的存在,我们就可以面对布朗假设的第二部分。对于质量比μ定值的每一个极限轨道,应该是两个周期振动族的头,对于第一类,周期随着雅可比常数的减小而减小,而对于第二类,周期随着雅可比常数的增大而增大。
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引用次数: 21
Analytical Determination of Characteristic Exponents 特征指数的解析测定
Pub Date : 1965-09-13 DOI: 10.1016/B978-1-4832-2729-0.50012-0
A. Bennett
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引用次数: 10
Parameter Hunting Procedures 参数查找过程
Pub Date : 1965-09-13 DOI: 10.1016/B978-1-4832-2729-0.50020-X
Bernard A. Glassman, Virginia C. Zvonkovich
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引用次数: 2
Effect of Initial Configurations on Libration Point Motion 初始构型对振动点运动的影响
Pub Date : 1965-09-13 DOI: 10.1016/B978-1-4832-2729-0.50011-9
Lynn E. Wolaver
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引用次数: 6
Efficient and Accurate Orbit Prediction for Very Long Periods of Time 有效和准确的轨道预测很长一段时间
Pub Date : 1965-09-13 DOI: 10.1016/B978-1-4832-2729-0.50019-3
A. G. Lubowe
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引用次数: 0
Resonances Affecting Motion Near the Earth-Moon Equilateral Libration Points 影响地月等边振动点附近运动的共振
Pub Date : 1965-09-13 DOI: 10.1016/B978-1-4832-2729-0.50010-7
J. Breakwell, R. Pringle
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引用次数: 22
Error Equations of Inertial Navigation with Special Application to Orbital Determination and Guidance 惯导定轨与制导的误差方程
Pub Date : 1965-09-13 DOI: 10.1016/B978-1-4832-2729-0.50018-1
B. Lange, B. Parkinson
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引用次数: 2
期刊
Progress in Astronautics and Rocketry
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