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1)  blade profile
叶型
1.
By using the FINE/Turbo analysis software of Numeca,the present paper numerical simulates the four original and their optimum blade profiles with three-dimensional computation,and compares the aerodynamic characteristics with different Mach numbers and different incidences.
采用Num eca的FINE/Turbo分析软件对4种原始叶型及其优化叶型进行了三维数值模拟,并对在不同马赫数与不同冲角下的气动性能作了比较。
2.
For investigating the profile that has advanced startup characteristic with the supersonic and transonic conditions, the present paper design the suction surface as the“concave”type based on a transonic profile,and analysis the changing of the aerodynamic characteristic of the original and the remodeled cascades,so gives a thoughtway for designing the blade profiles.
为了探索在超跨音速下具有优良启动特性的叶型,以某跨音速叶型为例,对吸力面作了“凹”形设计,分析比较了改型前后叶栅气动性能的变化,为叶型设计提供一种思路。
3.
To form software for design optimization of compressor blade profiles,the IGA is combined with the above blade profile parameterization and flow field calculation method.
将并行遗传算法与NS方程流场计算方法、Hicks-Henne函数叶型参数化方法结合构成叶型自动优化设计软件,软件可用于叶型设计和对已有叶型的改进。
2)  profile [英]['prəʊfaɪl]  [美]['profaɪl]
叶型
1.
The designed efficiency method of 7-40 sintering blower model using “equal deceleration flow model" is carried out, and compare the model with conventional designed through test research many times, the method of design and draw profile using "equal deceleration flow model" are obtained.
应用等减速流型进行了7-40烧结鼓风机模型的效率法设计,并通过与常规设计的模型进行多次对比试验研究,得出了应用等减速流型进行设计和叶型绘制方法,结果表明:应用等减速流型设计在提高模型效率方面有明显的效果。
2.
The aerodynamic characteristics of the profile NACA0015 with steady suction air on the profile surface have been investigated by numerical simulating the flow fields around the profile under different low Mach Numbers.
提高叶型升力,扩大其稳定工作范围一直是叶轮机械领域关心的问题。
3.
For understanding the aerodynamic characteristics of the blade cascade with aft-loading profiles, the experimental investigations were carried out on the low speed annular wind tunnel with the conventional straight blades and the curved blades cascades that have the aft-loading profiles.
为了对具有“后部加载”叶型叶栅的气动性能进行深入的了解 ,本文在环形叶栅低速风洞上对具有“后部加载”叶型的常规直叶片栅和弯叶片栅进行了吹风实验。
3)  Blade [英][bleɪd]  [美][bled]
叶型
1.
Blade Design Optimization System Based on Auto-Parallel Computa tion with JAVA RMI Implementation;
采用JAVA RMI实现自动并行计算的叶型优化设计平台
2.
Design research of supersonic fan blade profile
超声速风扇叶型设计研究
3.
Research on Optimization of High Subsonic Compressor Blades;
熟悉叶型优化及相关程序,总结当前压气机叶片优化设计所涉及各领域现状,分析本文研究意义。
4)  Blade airfoil
叶型
5)  blade shape
叶型
1.
Based on the research on the motion law of the drilling fluid along the blade, the necessary condition of the blade shape for a high efficiency turbodrill is obtained.
由此提出了一种满足条件的叶片型线模型,并根据叶片的几何关系给出了数学模型的求解方法,为提高现有涡轮钻具的工作效率提供了一种参考叶型
2.
TBM-6 type blade shape measure Instrument for hydraulic turbine runner and its application were introduced in this paper.
本文介绍了TBM-6型水轮机转轮叶型测绘仪及其应用情况。
3.
The research and application of the TBM-6 type blade shape measure Instrument for hydroturbine runner were introduced in this paper.
全面介绍了TBM-6型大型水轮发电机组水轮机转轮叶型测绘仪的开发、研制及应用情况。
6)  leaf type
叶型
1.
Determination of Protein Content in Different Leaf Types of Pinellia ternata
不同叶型半夏蛋白质含量测定
2.
The results indicate that more attention should be paid on increasing leaf length but keeping the present leaf curvature for leaf type,on increasing the thickness of basal internode and the length of the internode below panicle for stem type,and on increasing grains per panicle and branch number for panicle type in early season indica rice breeding.
以不同年代育成的28个代表性早籼稻品种为材料,在同一生态条件下种植,系统研究了叶型、茎型、穗型若干株型性状的演变特征。
补充资料:GS,GT型空心桨叶连续干燥机

 

 

 
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