wing area
英 [wɪŋ ˈeəriə]
美 [wɪŋ ˈeriə]
网络 翼面积; 机翼面积; 主翼面积
双语例句
- Welding in the wing fastening rail plug-weld the wing fastening rail in area using inert gas.
焊接翼子板固定横杆使用惰性气体通过塞焊将翼子板固定横杆焊接在区域中。 - The horizontal tail wing of the wing-in-ground effect craft has the advantages of great ascensional force, small area and low production cost.
这种地效翼船水平尾翼，升力大、面积小、生产成本低。 - The ratio of the weight of an airplane to its wing area.
机翼同飞机重量的比率。 - Case studies included the monitoring of the central wing and outer panel jointing area, the upper and lower pivots of main landing gears.
论文以中央翼-外翼连接区域和起落架上枢轴接头等关键部位为例，说明实施监测的方法。 - South Wing Jixian Coal Mine Five Coal Mining Area Underthe Extension of the New Design Verification
集贤煤矿南翼五层煤下延采区新设计方案论证 - With the increasing thickness of the west wing mining area and the whole year air heat release in tunnels, heat disaster will be more serious in summer.
随西翼采深的加大，井巷全年的风流放热，夏季西翼采区的热害将更加严重。 - The wing sails with 3.1 percentage of essential wing area have observable efficiency in reducing induced drag. The factors of the induced drag were reduced by 20 percent.
总面积为3.1%基本翼面积的翼尖帆片对减少诱导阻力具有明显效果，诱导阻力因子减小20%左右。 - Initial results from WING, the continuous GPS network in the western Pacific area
西太平洋地区连续GPS整体网络最初结果 - A predicting method of wing turbulent separation area and the influence of different turbulent models on the results of prediction are introduced.
介绍了机翼气流分离区的预测方法和不同湍流模型对其预测结果的影响。 - Solving the Rate of Wing Cross Sectional Area from Multiple Images
用多幅照片求取机翼面积率的方法 - Prediction of Wing Boundary Layer Separation Area With Turbulent Models
用不同湍流模型预测机翼边界层分离区 - Has designed the complete wing non-level ( NWL, Non-Wing-Level) automatic attack algorithm in view of the pitch open area forms of defensive action.
针对上仰空地攻击方式设计了完整的机翼非水平（NWL，Non-Wing-Level）自动攻击算法。 - The task of the initial sizing is to find the primary parameters of aircraft, including the takeoff wing loading, thrust-to-weight ratio, takeoff weight, wing area, aspect ratio of wing, wing sweep, thickness and taper ratio to match the mission requirements.
其任务是找到能满足飞机性能要求的飞机主要参数。这些参数包括：起飞翼载、推重比、起飞重量、机翼面积、机翼翼载、机翼后掠角、机翼相对厚度和机翼梯形比等。 - The area affected by two factors control the lithology and structure, lithologic reservoir development area mainly concentrated in the structure of the wing, furrow area, slope area.
本研究区受岩性和构造双重因素控制，岩性油气藏储层发育区主要集中在构造的翼部、深凹区、斜坡区。 - The size of fillet weld at the wing plate should be appropriate in the basic premise of the mechanical properties to reduce the weld cross-sectional area and reduce the heat input.
翼板处的焊角尺寸参数选用要得当，在保证其满足基本力学性能的前提下，适当的减少焊角尺寸，来减少焊缝的截面积，从而减少焊缝的热输入，减小变形值。