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排序方式: 共有190条查询结果,搜索用时 250 毫秒
51.
F.R. Klinkhamer 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012,49(1):213-221
A possible gluon-condensate-induced modified-gravity model with f(R) ∝ ∣R∣1/2 has been suggested previously. Here, a simplified version is presented using the constant flat-spacetime equilibrium value of the QCD gluon condensate and a single pressureless matter component (cold dark matter, CDM). The resulting dynamical equations of a spatially-flat and homogeneous Robertson-Walker universe are solved numerically. This simple empirical model allows, in fact, for a careful treatment of the boundary conditions and does not require a further scaling analysis as the original model did. Reliable predictions are obtained for several observable quantities of the homogeneous model universe. In addition, the estimator EG, proposed by Zhang et al. to search for deviations from standard Einstein gravity, is calculated for linear sub-horizon matter-density perturbations. The QCD-scale modified-gravity prediction for EG(z) differs from that of the ΛCDM model by about ±10% depending on the redshift z. 相似文献
52.
以氯化亚锡作显色荆,用分光光度法测定镀铂溶液中的铂,优选出最佳的测量波长。结果表明,铂的质量浓度介于0-10μg/ml范围内遵守比尔定律,本方法简便快捷,并具有良好的选择性,方法可用于镀铂溶液中的铂含量的测定。 相似文献
53.
为了研究液滴冲击移动液膜问题,建立了三维不可压缩层流计算模型,基于耦合的水平集-流体体积法对两相界面进行追踪,探讨了液膜速度和厚度、液滴直径和速度对冲击移动液膜过程的影响。研究表明:液膜静止时,冲击结果是对称的,而液膜移动时,冲击结果变为非对称;液膜速度对冠上游生长具有增强效应,而对冠下游具有抑制作用,增加液膜速度冠的上游高度增加、下游高度减小,内径增加;液膜厚度增加,液膜与壁面的粘性损失减小,吸收冲击动能的能力增强,当无量纲液膜厚度小于1时,冠的上、下游高度均随着液膜厚度的增加而增加,否则相反;当无量纲液膜厚度小于0.5时,冠内径随着液膜厚度的增加而增加,否则反之;随液滴直径和速度的增大,冠的高度和内径均增加。 相似文献
54.
55.
调节燃速和降低压力指数是RDX-CMDB推进剂性能改善的技术关键之一.用同一种有机铅、铜盐催化剂对实测比冲为2000~2200N·s/kg的四种双基及RDX-CMDB推进剂进行试验研究表明:铅-铜-炭黑三种燃烧催化剂组合使用也可在RDX-CMDB无烟推进剂中获得良好的平台或麦沙效应.这里炭黑的加入起了关键作用,可用燃烧催化的铅-碳理论作进一步的解释.所述的铅、铜催化剂与四种碳黑搭配,可使所研究的四种推进剂燃速在14~29mm/s范围内调节. 相似文献
56.
《中国航空学报》2020,33(3):1026-1036
A high resolution range profile (HRRP) is a summation vector of the sub-echoes of the target scattering points acquired by a wide-band radar. Generally, HRRPs obtained in a non-cooperative complex electromagnetic environment are contaminated by strong noise. Effective pre-processing of the HRRP data can greatly improve the accuracy of target recognition. In this paper, a denoising and reconstruction method for HRRP is proposed based on a Modified Sparse Auto-Encoder, which is a representative non-linear model. To better reconstruct the HRRP, a sparse constraint is added to the proposed model and the sparse coefficient is calculated based on the intrinsic dimension of HRRP. The denoising of the HRRP is performed by adding random noise to the input HRRP data during the training process and fine-tuning the weight matrix through singular-value decomposition. The results of simulations showed that the proposed method can both reconstruct the signal with fidelity and suppress noise effectively, significantly outperforming other methods, especially in low Signal-to-Noise Ratio conditions. 相似文献
57.
针对航天器相对姿态跟踪过程中严重的非线性及控制器设计的复杂性,建立了基于修正罗德里格斯参数的航天器相对姿态运动学和动力学方程并根据Lyapunov直接法设计了非线性前馈控制律.设计的控制律不仅保证闭环系统稳定,还使得航天器相对姿态跟踪误差快速收敛到零点邻域内.通过在Matlab/Simulink环境下对航天器相对姿态跟踪进行数值仿真,验证了建立模型和设计控制律的有效性. 相似文献
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59.
为了分析宽马赫数飞行条件下超声速燃烧室再生冷却性能以及考虑燃料高温裂解效应对冷却的影响,发展了具有一定通用性的超声速燃烧室再生冷却系统气-固-液传热分析模型,对燃烧室内流、冷却剂流动以及冷却结构进行了气-固-液传热耦合计算.燃烧室内流计算模型无需实验测量的静压数据以及总温/释热分布假设,通过直接求解质量、动量、能量守恒微分方程并结合燃料混合及燃烧模型来获得内流参数分布.同时对燃烧室壁面传热进行了计算,将冷却结构内冷却剂的流动、换热与燃烧室内流耦合,并且着重考虑了煤油作为冷却剂,其物态随温度、压力变化以及高温时出现的热/催化裂解吸热化学反应.基于实验数据发展了煤油热/催化裂解总包反应模型,对煤油热裂解和催化裂解两种过程的化学吸热性能进行了对比,研究了热/催化裂解效应对再生冷却的影响. 相似文献
60.
Christian Trenkel Steve Kemble Neil Bevis Joao Magueijo 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
We suggest that LISA Pathfinder, a technology demonstrator for the future gravitational wave observatory LISA, could be used to carry out a direct experimental test of Modified Newtonian Dynamics (MOND). The LISA Pathfinder spacecraft is currently being built and the launch date is just a few years away. No modifications of the spacecraft are required, nor any interference with its nominal mission. The basic concept is to fly LISA Pathfinder through the region around the Sun-Earth saddle point, in an extended mission phase, once the original mission goals are achieved. We examine various strategies to reach the saddle point, and find that the preferred strategy, yielding relatively short transfer times of just over 1 year, probably involves a lunar fly-by. LISA Pathfinder will be able to probe the intermediate MOND regime, i.e. the transition between deep MOND and Newtonian gravity. We present robust estimates of the anomalous gravity gradients that LISA Pathfinder should be exposed to, based on MONDian effects as derived from the Tensor-Vector-Scalar (TeVeS) theory. The spacecraft speed and spatial scale of the MOND signal combine in a way that the spectral signature of the signal falls precisely into LISA Pathfinder’s measurement bandwidth. We find that if the gravity gradiometer on-board the spacecraft achieves its currently predicted sensitivity, these anomalous gradients could not just be detected, but measured in some detail. 相似文献