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1.
含催化剂RDXCMDB推进剂燃烧机理研究   总被引:1,自引:0,他引:1  
利用常压DSC及TG/DTG,高压DSC,单幅照相和燃烧波温度分布测试技术对含RDX的复合改性双基推进剂(RDXCMDB)含和不含催化剂时的燃烧机理进行了研究,得到了该种推进剂在热分解和燃烧方面的一些重要结果。  相似文献   
2.
简要介绍Y19- 1 飞机飞行试验数据采集系统的组成和工作原理。着重阐述固态记录可编程采集编码器的特点  相似文献   
3.
探讨了胶黏剂黏度、硬铝表面处理方式及硅烷偶联剂KH-560的使用方式等因素对硬铝板/ZN-1阻尼材料复合结构件的粘接性能的影响。研究表明:如果硬铝板表面采用砂纸打磨处理时,采用黏度较低的TC-1环氧树脂胶或者在黏度较高的J-22环氧树脂胶中添加2%的硅烷偶联剂KH-560可以获得优异的粘接效果;当硬铝板表面采用铬酸阳极化处理时,两种胶黏剂均能获得优异的粘接效果。  相似文献   
4.
We have performed a spectral principal component analysis for a complete sample of 22 low redshift QSOs with spectra from Ly to H, and found three significant principal components, which account for 78% of the spectrum-to-spectrum variance. We present strong arguments that the first principal component represents the Baldwin effect, relating equivalent widths to the luminosity (i.e. accretion rate). The second component represents continuum variations, probably dominated by intrinsic reddening. The third principal component is directly related to broad emission-line width and X-ray spectral index, and therefore probably driven by Eddington accretion ratio, L/LEdd. The third set of relationships tie directly to the optical Principal Component 1 found by Boroson and Green [Boroson, T., Green, R.F., Astrophys. J. Suppl. 80, 109, 1992 (BG92)], and are the primary cause of scatter in the Baldwin relationships.  相似文献   
5.
本文给出了一个使滞后的相似组合大系统镇定的分散鲁棒控制器的设计方法。不确定性是时变的,是以不确定参数出现在每个子系统中,而存在于互联项中的不确定性假设可能知道它的边界,当系统具有某种特征时,简化了一般控制器的设计。  相似文献   
6.
This paper studies a nonlinear robust control algorithm of the electro-hydraulic load simulator (EHLS). The tracking performance of the EHLS is mainly limited by the actuator's motion disturbance, flow nonlinearity, and friction, etc. The developed controller is developed based on the nonlinear motion loading model. The problems of the actuator's disturbance and flow nonlinearity are considered. To address the friction problem, the friction model of the loading motor is identified experimentally. The friction disturbance is compensated using the obtained friction model. Therefore, this paper considers the main three factors comprehensively. The developed algorithm is easy to apply since the controller can be obtained just with one step back-stepping design. The stability of the developed algorithm is proven via Lyapunov analysis. Both co-simulation and experiments are performed to verify the effectiveness of this method.  相似文献   
7.
The evolution of luminous QSOs is linked to the evolution of massive galaxies. We know this because the relic black-holes found locally have masses dependent on the properties of the host galaxy’s bulge. An important way to explore this evolution would be to measure dependences of black-hole masses and Eddington accretion ratios over a range of redshifts, i.e., with cosmological age. For low redshift QSOs (and their lower luminosity Seyfert galaxy counterparts) it has been possible to infer black-hole masses from the luminosities and velocity dispersions of their host-galaxy bulges. These masses agree with those virial black-hole masses calculated from the Doppler widths of the broad Hβ emission lines. The latter method can then be extended to more distant and luminous QSOs, up to redshifts of 0.6 with ground-based optical observations. We discuss ways to extend these explorations to higher redshifts – up to 3 using the widths of QSOs’ broad UV emission lines, and in principle, and to redshifts near 4 from ground-based infrared observations of rest-frame Hβ at 2.5 μm. We discuss the possibility of investigating the accretion history of the higher redshift QSOs using measures of Eddington accretion ratio – the soft X-ray spectral index and the eigenvectors of Principal Components Analyses of QSOs’ UV emission-line spectra.  相似文献   
8.
90°强曲率弯管内三维湍流流场的数值分析   总被引:1,自引:0,他引:1  
席光  尚虹  王尚锦 《航空动力学报》1992,7(3):223-225,290
本文根据作者发展的一种能计算任意截面形状 90°弯管内三维不可压缩湍流流场的分析方法,利用作者实验的圆截面弯管数据 ( Rc/D=0.87)检验 k- ε双方程湍流模型预示强曲率三维湍流流场的精度。计算了 Rc/D=2.3的矩形截面和 Rc/D=0.87的圆截面 90°弯管,并将计算结果与相应实验数据进行了比较分析。结果表明,即使对曲率很强的弯管,吸力面 (内侧壁 )不出现二次流迁移所形成的低速区前,标准 k- ε双方程模型仍能较好地预示出平均速度场。   相似文献   
9.
Traditional hydraulic brake systems require a complex system of pipelines between an aircraft engine driven pump (EDP) and brake actuators, which increases the weight of the aircraft and may even cause serious vibration and leakage problems. In order to improve the reliability and safety of more electric aircraft (MEA), this paper proposes a new integrated self-powered brake system (ISBS) for MEA. It uses a hydraulic pump geared to the main wheel to recover a small part of the kinetic energy of a landing aircraft. The recovered energy then serves as the hydraulic power supply for brake actuators. It does not require additional hydraulic source, thus removing the pipelines between an EDP and brake actuators. In addition, its self-powered characteristic makes it possible to brake as usual even in an emergency situation when the airborne power is lost. This paper introduces the working principle of the ISBS and presents a prototype. The mathematical models of a taxiing aircraft and the ISBS are established. A feedback linearization control algorithm is designed to fulfill the anti-skid control. Simulations are carried out to verify the feasibility of the ISBS, and experiments are conducted on a ground inertia brake test bench. The ISBS presents a good performance and provides a new potential solution in the field of brake systems for MEA.  相似文献   
10.
严航  叶尚福  朱珍珍 《宇航学报》2013,34(4):531-538
针对TDMA多时隙信号不连续,通信时隙外噪声以及其它用户信号影响时/频差参数估计的问题,首先证明了多时隙多普勒频差信号具有相参性,指出多时隙信号在相关处理中能量是可以积累的;在此基础上,根据通信时隙外噪声、其它用户信号与特定用户信号在时域上的可分离特性,提出基于解调分选的TDMA时/频差参数估计方法,并推导分析了该方法的处理性能。试验结果表明,提出的方法可以实现TDMA信号中多用户信号的时/频差参数联合估计,可以有效降低通信时隙外噪声与其它用户信号对参数估计精度的影响。  相似文献   
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