涡轮叶片的循环蠕变分析

研究了航空发动机一级涡轮叶片的蠕变行为。对叶片的危险区作了静载恒温蠕变计算和变温变载蠕变计算。其结果是静载恒温蠕变和实验结果一致;其循环蠕变变形略小于静蠕变变形。变温变载下叶片的蠕变寿命可用静载恒温蠕变进行预估。      

A study on TEC reduction during the tail phase of the 21st June 2020 annular solar eclipse

Ionospheric response during the annular solar eclipse of June 21, 2020, has been examined in terms of the Total Electron Content (TEC) obtained from six Global Positioning System (GPS) receivers positioned in the Chinese-Taiwanese region. We have shown TEC variation from satellites designated by PRNs (Pseudo-Random Noise code) 2, 6, and 19. PRN wise TEC trend was observed to depend upon satellite-pass trajectory to the receiver's location during the eclipse period. A time lag of ~15–30 min is also observed in maximum TEC decrement after the phase of maximum eclipse. Instead of the percentage of eclipse magnitude, a reduction in TEC is seen more for the station for which the orbital track of respective satellites was in closer view relative to receivers for more hours of eclipse window. Additionally, the eclipse day diurnal variations are compared with the pre-eclipse day TEC trend, and observed results show a clear decrease in TEC values at all chosen stations after the eclipse onset then reached the lowest value a few minutes afterward the maximum eclipse phase.     

V形前缘对激波入射边界层流动影响的数值模拟与分析

为指导V形溢流唇口下游的进气道内部流动分析，采用数值模拟开展V形尖前缘对二维斜激波入射平板边界层流动的影响研究。以气流偏转角6°的二元楔面为基准激波发生器，设计了展向气流收缩角α(0°~60°, 0°对应二元构型)的V形前缘构型，开展对比研究。结果表明，V形前缘构型使得激波入射位置沿展向不均匀、流动具有明显三维特征，并且干扰区壁面压强上升、分离区尺度明显增大。在α=0°~60°范围内，干扰区流动的不均匀程度、分离区尺度随α增大单调增加。进一步分析表明，V形前缘构型干扰具有中间平直、侧边斜掠的耦合入射特性，体现为对称面壁面压强符合自由干扰理论，侧边斜掠入射区参数符合斜掠干扰的锥形流特征。对比二元与α=45°构型的无粘模拟结果，V形前缘会诱导展向两侧对称的斜掠激波、并在对称面相互干扰产生平直的“桥”激波，这使得激波入射位置沿展向不均匀并偏向下游。其中对称面处平直入射激波压升比(2.49)高于二元构型结果(2.24)，侧边斜掠激波强度与二元构型基本一致。这些因素综合导致V形前缘构型的分离尺度增大。     

SAMI2 model results for the quiet time low latitude ionosphere over India

Efficacy of SAMI2 model for the Indian low latitude region around 75°E longitudes has been tested for different levels of solar flux. With a slight modification of the plasma drift velocity the SAMI2 model has been successful in reproducing quiet time ionospheric low latitude features like Equatorial Ionization Anomaly. We have also showed the formation of electron hole in the topside equatorial ionosphere in the Indian sector. Simulation results show the formation of electron hole in the altitude range 800–2500?km over the magnetic equator. Indian zone results reveal marked differences with regard to the time of occurrence, seasonal appearances and strength of the electron hole vis-a-vis those reported for the American equatorial region.     

涡桨教练机螺旋桨设计关键技术分析

涡桨教练机以其完美的节油特性越来越受用户青睐,本文就涡桨教练机推进部件螺旋桨的设计技术进行探讨。简要介绍了提高螺旋桨效率的一般技术,重点围绕提高螺旋桨效率以及影响全机气动特性的关键技术展开分析。     

The Indian EO Programme-national and global drivers

The Indian Earth Observations Program, over the past three decades, has been mainly driven by the national need for natural resources management, environment monitoring and disaster support. With an array of seven Indian Earth Observation Satellites, national development support has been provided through a well-knit institutional framework of a National Natural Resources Management System (NNRMS). A wide variety of applications have been developed as an inter-agency effort over the past 15 years. Now, the capacity of the programme has extended into the global arena and is providing operational data services to the global user community. Positioning of relevant policy guidelines for the EO program to contribute to national endeavor and its transitioning for global outreaching and development of a commercial enterprise — both at national and global levels has been an area of constant attention within ISRO.Issues related to defining the space and data acquisition as a national “public ground”, costing of data products and services and evolving a commercial Earth Observation policy have been addressed for providing the overall thrust of the Indian Earth Observations program. The paper discusses the evolution of the policy in the early stages and its transition today to support a two-pronged strategy of supporting national development support and at the same time, developing a commercial program. The paper also illustrates the success of these policy endeavors through specific cases of applications and development of value added services. The paper also brings out the potential policy adjustments that will be called for in the coming years.     

New approach for suppression of FM jamming in GPS receivers

A new approach is proposed for the suppression of FM jammers in C/A code GPS receivers. This approach is based on the cascading of the augmented-state approximate conditional mean (ASACM) filter and the discrete wavelet transform (DWT) filter. An ASACM filter for single interference suppression in spread-spectrum systems has been reported in the recent literature. However, the formulation of the ASACM filter and its performance analysis is lacking in the case of suppression of multiple FM interferences. The ASACM filter is formulated here for the suppression of multiple FM jammers. Further, a DWT filter using biorthogonal wavelet is suggested for the suppression of FM jammers. Finally, these two filters are cascaded to get an optimum performance for higher jammer to signal ratio, which is of importance in the GPS, for the case of suppression of multiple FM jammers. The performance of the proposed filters is analyzed through simulation examples for the suppression of single and multiple FM jammers in GPS receivers     

Reduction of Positional Estimate Errors in HF Hyperbolic Position-Fixing Systems

A simple ionospheric prediction model is employed to determine the reduction in the positional estimate errors in HF hyperbolic position-fixing systems provided by the use of the model. Quantitative results of positional estimate errors before and after the application of the model to experimental time-delay data are compared.     

二进码的复制特性

本文基于复制理论的思想,分析了有关的二进码,指出了二进码本身具有的某种复制特性,并且根据组合思想提出了新的二进码—K码,根据平移复制和对称复制的等效性,证明了K码和自然码的关系,揭示了K码的物理意义.     

DZ22多孔板蠕变有限元与试验研究

本文选用航空发动机涡轮叶片用正交各向异性材料 DZ2 2在不同温度下进行蠕变三阶段试验 ,拟合出能反映三阶段蠕变的本构方程。利用试验结果验证了有限元程序分析正交各向异性材料蠕变的有效性。然后 ,针对气冷叶片的特点 ,探讨多孔构件的简化蠕变有限元分析方法。经对密布小孔板状试件的试验与有限元对比分析 ,两者结果吻合较好。