骚扰
发表于 2025-3-26 22:53:27
Otto Spaniolturing and handling difficulties, coupled with the tendency of their critical current densities to degrade rapidly under stress, have generally restricted their use to fairly straightforward, usually small-scale solenoidal-magnet applica tions. Likewise the Al5 compound VGa, which has a wider criti
远足
发表于 2025-3-27 01:27:48
J. P. Peltier,J. Zeyonsve ones, detailed discussion of which begins in Chapter 10. If treated phenomenologically as simply a “temperature-dependent property,” thermal expansion could be considered almost anywhere among the physical-property chapters of this book; if treated as a “thermal property,” it could logically be a
inventory
发表于 2025-3-27 05:24:32
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使成整体
发表于 2025-3-27 11:56:27
Flaminio Borgonovo,Luigi Frattadel) methods play the most important role, since they have the flexibility to accommodate a wide range of hazard function forms. Still, parametric methods have a place in biomedical research, and may be appropriate when survival data can be shown to approximately follow a particular parametric form.
符合国情
发表于 2025-3-27 17:26:58
Thomas E. Stern and we also introduced a parameter . that indexes the difference between the two survival distributions via the Lehmann alternative, .. Using Eq. 2.2.1 we can see that we can re-express this relationship in terms of the hazard functions, yielding the ., . This equation is the key to quantifying the
惊奇
发表于 2025-3-27 21:04:04
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minion
发表于 2025-3-28 01:21:42
Patrick F. Baker reality, and whether it is possible to enhance the sense of presence by reproducing the feeling of distance in environment that each of audience can easily build. The basic idea is from the needs of the times: the increase in online events due to the spread of COVID-19, and the loss of sense of dis
groggy
发表于 2025-3-28 05:12:35
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安定
发表于 2025-3-28 08:13:14
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轻弹
发表于 2025-3-28 14:10:07
P. Tran-Gia,Th. Stockstem. The plunge and pitch motion of this 2-D airfoil is controlled by trailing- and leading-edge control flaps. All of the model parameters are assumed to be unknown. The uncontrolled airfoil shows limit cycle oscillations (LCOs) if the freestream velocity exceeds certain specific value. First, an