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181.
Magnesium (Mg) alloys have broad application prospects in the fields of aerospace, national defense, and military industries, owing to their advantages of high specific strength and stiffness, good damping properties, and excellent castabilities. However, defects such as oxidation inclusions, shrinkage cavities and porosities, and hot cracks are readily generated in Mg alloy components, which seriously reduce the performance stability of the products. Related repair welding technologies for Mg alloys can greatly reduce the rejection rate and production cost, and exhibit significant value in scientific research and engineering application. In this review, the weldability of Mg alloys is introduced firstly according to their physical and chemical properties. Then, various repair welding technologies and pre-weld treatments applicable to Mg alloys are systematically summarized, and the effects of welding parameters as well as heat treatments on the microstructure and performance of the repaired joints are clarified. Finally, the existing problems and development trends of repair welding technologies for Mg alloys are summarized based on the actual engineering application requirements.  相似文献   
182.
In the space experiment "Molecular adaptation strategies of microorganisms to different space and planetary UV climate conditions" (ADAPT), bacterial endospores of the highly UV-resistant Bacillus subtilis strain MW01 were exposed to low-Earth orbit (LEO) and simulated martian surface conditions for 559 days on board the European Space Agency's exposure facility EXPOSE-E, mounted outside the International Space Station. The survival of B. subtilis MW01 spores from both assays (LEO and simulated martian conditions) was determined by a colony-formation assay after retrieval. It was clearly shown that solar extraterrestrial UV radiation (λ≥110?nm) as well as the martian UV spectrum (λ≥200?nm) was the most deleterious factor applied; in some samples only a few spore survivors were recovered from B. subtilis MW01 spores exposed in monolayers. However, if shielded from solar irradiation, about 8% of MW01 spores survived in LEO conditions, and 100% survived in simulated martian conditions, compared to the laboratory controls. The results demonstrate the effect of shielding against the high inactivation potential of extraterrestrial solar UV radiation, which limits the chances of survival of even the highly UV-resistant strain of B. subtilis MW01 in the harsh environments of outer space and the martian surface.  相似文献   
183.
双组元高室压脉冲火箭发动机工作特性分析   总被引:2,自引:1,他引:1  
为了研究高室压脉冲火箭发动机的工作特性,在分析其工作原理的基础上建立了数学模型,其中燃烧室和挤压腔采用零维模型,喷管采用一维准稳态模型,采用四阶Runge-Kutta法进行了求解.结果表明,燃烧室的最大压强和平均压强都高于推进剂供给压强,而挤压过程中进出燃烧室的质量不守恒是压强升高的原因.与常规液体火箭发动机相比较表明,脉冲火箭发动机的真空比冲提高了7.5%,而喉部面积仅为其10.2%.  相似文献   
184.
Massive stars, at least \(\sim10\) times more massive than the Sun, have two key properties that make them the main drivers of evolution of star clusters, galaxies, and the Universe as a whole. On the one hand, the outer layers of massive stars are so hot that they produce most of the ionizing ultraviolet radiation of galaxies; in fact, the first massive stars helped to re-ionize the Universe after its Dark Ages. Another important property of massive stars are the strong stellar winds and outflows they produce. This mass loss, and finally the explosion of a massive star as a supernova or a gamma-ray burst, provide a significant input of mechanical and radiative energy into the interstellar space. These two properties together make massive stars one of the most important cosmic engines: they trigger the star formation and enrich the interstellar medium with heavy elements, that ultimately leads to formation of Earth-like rocky planets and the development of complex life. The study of massive star winds is thus a truly multidisciplinary field and has a wide impact on different areas of astronomy.In recent years observational and theoretical evidences have been growing that these winds are not smooth and homogeneous as previously assumed, but rather populated by dense “clumps”. The presence of these structures dramatically affects the mass loss rates derived from the study of stellar winds. Clump properties in isolated stars are nowadays inferred mostly through indirect methods (i.e., spectroscopic observations of line profiles in various wavelength regimes, and their analysis based on tailored, inhomogeneous wind models). The limited characterization of the clump physical properties (mass, size) obtained so far have led to large uncertainties in the mass loss rates from massive stars. Such uncertainties limit our understanding of the role of massive star winds in galactic and cosmic evolution.Supergiant high mass X-ray binaries (SgXBs) are among the brightest X-ray sources in the sky. A large number of them consist of a neutron star accreting from the wind of a massive companion and producing a powerful X-ray source. The characteristics of the stellar wind together with the complex interactions between the compact object and the donor star determine the observed X-ray output from all these systems. Consequently, the use of SgXBs for studies of massive stars is only possible when the physics of the stellar winds, the compact objects, and accretion mechanisms are combined together and confronted with observations.This detailed review summarises the current knowledge on the theory and observations of winds from massive stars, as well as on observations and accretion processes in wind-fed high mass X-ray binaries. The aim is to combine in the near future all available theoretical diagnostics and observational measurements to achieve a unified picture of massive star winds in isolated objects and in binary systems.  相似文献   
185.
Ceylan  Savas  van Driel  Martin  Euchner  Fabian  Khan  Amir  Clinton  John  Krischer  Lion  Böse  Maren  Stähler  Simon  Giardini  Domenico 《Space Science Reviews》2017,211(1-4):595-610

The InSight mission will land a single seismic station on Mars in November 2018, and the resultant seismicity catalog will be a key component for studies aiming to understand the interior structure of the planet. Here, we present a preliminary version of the web services that will be used to distribute the event and station metadata in practice, employing synthetic seismograms generated for Mars using a catalog of expected seismicity. Our seismicity catalog consists of 120 events with double-couple source mechanisms only. We also provide Green’s functions databases for a total of 16 structural models, which are constructed to reflect one-dimensional thin (30 km) and thick (80 km) Martian crust with varying seismic wave speeds and densities, combined with two different profiles for temperature and composition for the mantle. Both the Green’s functions databases and the precomputed seismograms are accessible online. These new utilities allow the researchers to either download the precomputed synthetic waveforms directly, or produce customized data sets using any desired source mechanism and event distribution via our servers.

  相似文献   
186.
The NASA InSight mission will provide an opportunity for soil investigations using the penetration data of the heat flow probe built by the German Aerospace Center DLR. The Heat flow and Physical Properties Probe (HP3) will penetrate 3 to 5 meter into the Martian subsurface to investigate the planetary heat flow. The measurement of the penetration rate during the insertion of the HP3 will be used to determine the physical properties of the soil at the landing site. For this purpose, numerical simulations of the penetration process were performed to get a better understanding of the soil properties influencing the penetration performance of HP3. A pile driving model has been developed considering all masses of the hammering mechanism of HP3. By cumulative application of individual stroke cycles it is now able to describe the penetration of the Mole into the Martian soil as a function of time, assuming that the soil parameters of the material through which it penetrates are known. We are using calibrated materials similar to those expected to be encountered by the InSight/HP3 Mole when it will be operated on the surface of Mars after the landing of the InSight spacecraft. We consider various possible scenarios, among them a more or less homogeneous material down to a depth of 3–5 m as well as a layered ground, consisting of layers with different soil parameters. Finally we describe some experimental tests performed with the latest prototype of the InSight Mole at DLR Bremen and compare the measured penetration performance in sand with our modeling results. Furthermore, results from a 3D DEM simulation are presented to get a better understanding of the soil response.  相似文献   
187.
Clinton  J.  Giardini  D.  Böse  M.  Ceylan  S.  van Driel  M.  Euchner  F.  Garcia  R. F.  Kedar  S.  Khan  A.  Stähler  S. C.  Banerdt  B.  Lognonne  P.  Beucler  E.  Daubar  I.  Drilleau  M.  Golombek  M.  Kawamura  T.  Knapmeyer  M.  Knapmeyer-Endrun  B.  Mimoun  D.  Mocquet  A.  Panning  M.  Perrin  C.  Teanby  N. A. 《Space Science Reviews》2018,214(8):1-51
Space Science Reviews - In recent decades, volcanic and cryovolcanic activity on moons within the Solar System has been recognised as an important source of cosmic dust. Two moons, Jupiter’s...  相似文献   
188.
碳氢燃料流向涡掺混超燃模型燃烧室冷态流场数值研究   总被引:1,自引:0,他引:1  
对一种超声速燃烧模型燃烧室的冷态流场进行了数值研究。为稳定超燃火焰并提高燃烧速率和效率,取少量的冲压空气进行稳定的亚燃预燃烧,并以之作为超燃室的一个稳定火炬,其高温燃气将吸热型碳氢燃料预先蒸发汽化并部分裂解为短链小分子,最后通过城墙波瓣掺混器形成的流向涡带入超声速主流,以期实现快速高效的超燃燃烧。计算结果表明:首先,城墙波瓣掺混器能够在较小总压损失下得到显著掺混效果;其次,本文从气动结构的角度专门探究了亚/超燃接力阶段较低的隔离段进口马赫数存在热堵塞的可能性,发现较难适宜超燃启动点火。  相似文献   
189.
B2-RuAl合金中原子扩散的第一原理计算   总被引:1,自引:0,他引:1  
采用第一原理赝势平面波方法,计算B2-RuA l合金中Ru和A l在不同情况下的扩散,用扩散激活能有效地表述和研究其化学反应的难易。计算发现:在空位扩散时,A l原子要比Ru原子容易扩散,即Ru原子比A l原子更稳定一些;当考虑不同扩散浓度和周边原子影响的情况时,也是A l原子要比Ru原子容易扩散,但其扩散激活能不同,所以在对B2-RuA l合金的原子扩散能计算时,周边的原子影响较大,我们应该考虑模型的尺寸效应。而比较不同扩散浓度下的扩散激活能,高浓度的扩散要难于低浓度。  相似文献   
190.
Liulin-5 is a particle telescope developed for the investigation of the radiation environment within the Russian spherical tissue-equivalent phantom on the International Space Station (ISS). Liulin-5 experiment is conducted aboard the Russian segment of ISS since 28 June 2007 as an adherent part of the international project MATROSHKA-R. The main objective of Liulin-5 experiment is to study the depth-dose distribution of the different components of the orbital radiation field in a human phantom. Additional objectives are mapping of the radiation environment in the phantom and its variations with time and orbital parameters (such as solar cycle, solar flare events, inclination and altitude). Liulin-5 is an active instrument, capable to provide real-time radiation data for the particle flux and dose rates, energy deposition and LET spectra. Data are recorded automatically on memory cards, periodically transported to ground by returning vehicles. In this report we present some first results from data analysis including energy deposition spectra, absorbed dose, dose rate and flux distribution measured simultaneously at 3 different depths of phantom’s radial channel and linear energy transfer (LET) spectrum. Data discussed are for the period July 2007–April 2008.  相似文献   
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