The interlayer gliding fault possesses the characteristics of deep- extension, low- angle, dip- slip, bed- zoned structure.

研究表明該類礦床賦存于中生代盆地蓋層與變質(zhì)基底接觸帶附近的低角度層間滑動(dòng)斷層中国内黄色网站在线，該斷層帶具有延伸大婷婷久久香蕉五月综合加勒比、低角度亚洲色图偷、傾向滑動(dòng)和層帶結(jié)構(gòu)等特征欧美三级国产一级。

A method was proposed for approaching the glide trajectories based on nsegment constant gliding angle.

提出用包含地球旋轉(zhuǎn)效應(yīng)的n個(gè)常滑翔角飛行段近似實(shí)際滑翔飛行軌跡的方法国产主播在线小蝌蚪。

The low- angle interlayer- gliding fault provided structure and physical- chemical conditions to ore- forming processes.

低角度層間滑動(dòng)斷裂帶為金礦成礦提供了十分有利的構(gòu)造和物理化學(xué)條件

Flight with the wind requires a shallower gliding angle on flatter wings.

在風(fēng)中飛行時(shí)要求有一個(gè)小的滑行角度精品综合日韩久久久久久久，使翅膀達(dá)到一個(gè)滿意的姿勢(shì)。

The dragonfly wing achieves large lift-drag ratio at the gliding range angle of attack.

我想問(wèn)題可能跟作者在模型選取得考慮有些關(guān)系国产日韩成人香蕉软件下载大全视频，另外似乎還是應(yīng)該考慮湍流的作用A级日本一线www。

Flight ; Approximate solution ; Constant gliding angle ; Longitudinal ; Long-range ; Long-time

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The approach to calculating the gliding angle and flight time of each segment was given.The procedure for approaching the whole glide trajectory was described.Two examples show that the differences in the gliding range and flight time between the approximate solution and the...

文中算例結(jié)果表明，該近似求解方法計(jì)算得到的滑翔航程和滑翔時(shí)間與實(shí)際值相差很小男人抽插女人免费看黄色网站，航程誤差率約為0.7%aaa湿湿湿，時(shí)間誤差率約為0.6%，因此該方法在近似小初始滑翔角的長(zhǎng)航時(shí)遠(yuǎn)程縱向滑翔飛行時(shí)是有效的、可行的色黄网站在线播放，尤其針對(duì)航程在地球半圈以上的滑翔飛行軌跡国产美女一级A片免费观看9。

The energy exchange analysis indicates that gliding energy efficiency is dependant on the lift drag ratio of the wings and gliding angle of the hull. Through the calculation in this thesis, it can be concluded that enhancing the lift drag ratio can largely improve the energy efficiency when the gliding angle is in the range of 10to 40 degree, and when lift drag ratio is fixed, there exists a special gliding angle for the maximum of the efficiency, which provide theoretical basis for the design of operating parameters.

通過(guò)能量轉(zhuǎn)換分析，得出滑翔機(jī)航行效率由機(jī)翼升阻比和機(jī)身航行角決定操操日日日操，航行角在10~40度范圍內(nèi)，增大機(jī)翼升阻比可顯著提高航行效率久久国产一区精品免费观看；并由計(jì)算得出一级黄色一级黄色一级黄色一级黄色a级毛片，在升阻比一定的情況下，總存在一個(gè)使滑翔機(jī)航行效率達(dá)到最大的航行角度亚洲熟妇AⅤ无码一区二区，為樣機(jī)工作參數(shù)設(shè)計(jì)提供了理論依據(jù)黄片AAAAAAAAAAAAA。