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61.
62.
63.
凸轮检测方法的误差分析 总被引:2,自引:0,他引:2
刘兴富 《航空精密制造技术》1998,(6)
对发动机凸轮检测方法的原理误差、检测系统误差、测头制造及安装误差、凸轮偏心误差、阿贝误差及检测方法总误差等进行了比较全面的分析 相似文献
64.
E. Bering M. Engebretson R. Holzworth A. Kadokura M. Kokorowski B. Reddell J. Posch H. Yamagishi 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009
The 2nd Polar Patrol Balloon campaign (2nd-PPB) was carried out at Syowa Station in Antarctica during 2002–2003. Identical stratospheric balloon payloads were launched as close together in time as allowed by weather conditions to constitute a cluster of balloons during their flights. A very pronounced negative ion conductivity enhancement was observed at 32 km in the stratosphere below the auroral zone on 27 January 2003 from 1500 to 2200 UT. During this event, the conductivity doubled for an interval of about 7 h. This perturbation was associated with an extensive Pc 1 or Pi 1 wave event that was observed by several Antarctic ground stations, balloon PPB 10, and the Polar spacecraft. No appreciable X-ray precipitation was observed in association with this event, which would point to >60 Mev proton precipitation as a possible magnetosphere–stratosphere coupling mechanism responsible for the conductivity enhancement. Such precipitation is consistent with the wave data. During the latter half of the event, Ez was briefly positive. There was a tropospheric Southern Ocean storm system underneath the balloon during this interval. If the event was associated with this storm system and not energetic proton precipitation, the observations imply an electrified Southern Ocean storm and major perturbations in stratospheric conductivity driven by a tropospheric disturbance. This event represents a poorly understood source for global circuit current. Precipitating energetic proton data from Akebono and NOAA POES spacecraft show significant >16 MeV precipitation was occurring at the location of PPB 8 but not PPB 10, suggesting that proton precipitation was, in fact, the responsible coupling mechanism. 相似文献
65.
Sergey Pulinets Dmitry Davidenko 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
The electromagnetic coupling between the seismically activated area and the ionosphere is considered within the framework of the Global Electric Circuit (GEC) conception. First we consider the anomalous variations in the ionosphere associated with the earthquake preparation process, their temporal and spatial characteristics using the results from recent publications. Then the GEC conception is presented shortly with main accent put on ionization processes which play key role in the complex chain of physical and chemical interactions changing the electric properties of the planetary boundary layer of atmosphere. We treat this part of troposphere as an open complex system with dissipation where so called “blow up” processes are developed leading to sharp and fast changes of atmospheric parameters including the electric properties of the boundary layer. The new concept named Spatial Scintillation Index is introduced in the last part of the paper. In general, this paper may be considered as a short review of the recent achievements in understanding of the seismo-ionospheric coupling. 相似文献
66.
采用熔铸法制备CuNiAl合金,Cu含量为95wt%,Ni/Al原子比分别为1:3、1:2、1:1、2:1、3:1的CuNiAl合金。利用涡流电导仪和磨损试验机测量了不同状态合金的导电率。研究发现:CuNiAl合金随着Ni含量的逐渐增加,导电率减小,合金的黏着磨损减弱,磨粒磨损现象明显增加。 相似文献
67.
《中国航空学报》2020,33(5):1541-1548
Uni-directional carbon/carbon composites with high thermal conductivity are suitable to supply continuous thermal protection for future reentry vehicles since they could reduce surface temperature and ablation rates simultaneously in harsh environments. In this work, the high thermal conductivity carbon/carbon composites were prepared by chemical vapor infiltration. After heat-treatment, both their open porosity and internal friction increase due to the fiber/matrix thermal expansion mismatch; while their thermal conductive performance become better due to more complete carbon structure. With raising heat-treatment temperature from 1800 °C to 2450 °C, the mass and linear ablation rates of C/C composites with fibers vertical to the oxyacetylene torch for 60 s decrease from 0.66 mg/s and 2.95 μm/s to 0.51 mg/s and 2.05 μm/s respectively. The improved ablation resistance is resulted from the increased thermal conductivity from 282 to 508 W/(m·K) and more carbon fibers exposed to the flame during ablation, which have better oxidation resistance than those of carbon matrix. While such ablation rates become larger for composites with fibers parallel to the flame, from 1.02 mg/s and 3.73 μm/s to 1.28 mg/s and 5.01 μm/s respectively since the ablation occurred more easily through gaps at the fiber/matrix interfaces, which become larger and are always exposed to the flame for this case. 相似文献
68.
针对钼钛锆这一耐高温材料在航天动力系统中的特殊加工需求,开展了电火花加工钼钛锆合金的工艺特性研究.采用DOE的方法,设计了25-1析因试验对放电参数进行筛选,得到对加工效果有显著影响的3个参数;在此基础上设计了响应曲面试验,探讨了包括脉宽、占空比和峰值电流等放电参数对材料去除率和电极相对损耗率的影响,并且拟合得到了材料去除率和相对电极损耗率的推荐公式和响应曲面图.通过分析试验结果表明:(1)材料去除率受峰值电流变化的影响最明显,并且脉宽与占空比呈现一定的交互关系;(2)电极相对损耗率受峰值电流变化影响不明显,受脉宽和占空比变化影响大,而且两者呈现一定的交互关系. 相似文献
69.
C.M. Denardini H.C. Aveiro J.H.A. Sobral J.V. Bageston L.M. Guizelli L.C.A. Resende J. Moro 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
Zonal and vertical electric fields were estimated at E region heights in the Brazilian sector. Zonal electric fields are obtained from the vertical electric fields based on their relation through the Hall-to-Pedersen ionospheric conductivities ratio. The technique for obtaining the vertical electric field is based on its proportionality to the Doppler velocities of type 2 irregularities as detected by coherent radars. The 50 MHz backscatter coherent (RESCO) radar was used to estimate the Doppler velocities of the type 2 irregularities embedded in the equatorial electrojet. A magnetic field-line integrated conductivity model was developed to provide the conductivities. It considers a multi-species ionosphere and a multi-species neutral atmosphere, and uses the IRI 2007, the MISIS 2000 and the IGRF 10 models as input parameters for ionosphere, neutral atmosphere and Earth’s magnetic field, respectively. The ion-neutral collision frequencies of all the species are combined through the momentum transfer collision frequency equation, and different percentages of electron-neutral collisions were artificially included for studying the implication of such increase in the zonal electric field, which resulted ranging from 0.13 to 0.49 mV/m between the 8 and 18 h (LT), under quiet magnetic conditions. 相似文献
70.
High-efficiency aircraft antiskid brake control algorithm via runway condition identification based on an on-off valve array 总被引:1,自引:1,他引:1
The aircraft antiskid braking system is an important hydraulic system for preventing tire bursts and ensuring safe take-off and landing. The brake system adjusts the force applied on the brake discs by controlling the brake pressure. Traditional aircraft antiskid braking systems achieve antiskid performance by controlling the braking pressure with an electrohydraulic servo valve. Because the pilot stage of an electrohydraulic servo valve is easily blocked by carbonized hydraulic oil, the servo valve would become a dangerous weak point for aircraft safety. This paper proposes a new approach that uses an on-off valve array to replace the servo valve for pressure control. Based on this new pressure control component, an efficient antiskid control algorithm that can utilize this discontinuous feature is proposed. Furthermore, the algorithm has the ability to identify the runway circumstances. To overcome the discontinuity in the process of using an on-off valve array, the Filippov framework is introduced. The conditions of convergence of the system are also discussed. The results of the digital simulations and the hardware-in-the-loop (HIL) braking experiments are used to verify the efficiency and stability of the proposed control algorithm. The method also proves that the on-off valve array can replace the servo valve perfectly as a new type of antiskid braking pressure control component. 相似文献