然后对这些气体的浓度增升进行分析，以得出某个给定表面区域所释放的气体量。
Rising concentrations of these gases are then analysed in order to draw conclusions about the amount of gas being given off by a given surface area.
所有音程也可用减(降半音)或增(升半音)来描述。
All intervals may also be qualified as diminished (a half step or semitone lower), or augmented (a half step or semitone higher).
本文使用数值模拟方法研究了吸气效应对分离的控制及增升作用。
The suction effect on separation and lift force are studied by numerical method.
风洞试验表明，改装成功的验证机增升装置具有良好的气动特性。
Wind tunnel tests indicate that the designed high lift system has good aerodynamics characteristics.
本文给出了飞机增升装置气动力特性的数值计算方法和计算结果。
This paper presents the numerical simulation method and calculation results for the flow around a high lift devices of airplane.
为进行超临界机翼气动设计技术的飞行验证，将某教练机改装为飞行验证机，为此必须进行增升装置的重新设计。
In order to validate the philosophy and software of supercritical wing design, a training plane is refitted and its high lift system is redesigned.
用低速风洞测力试验和襟翼处绕流的PIV测量试验研究锯齿形格尼襟翼在不同偏角下的增升效益。
Force and PIV local flow measurements were conducted in a low speed wind tunnel to study the effectiveness of serrated Gurney flap at different deflections.
由于高原隆升、全球气候增暖幅度不断增加，气候的持续干旱将是藏北大湖区未来气候的主要特征。
Owing to plateau building-up and the warmer of the global climate a, the continuing drought climate will be the main features of the northern Qinghai-Tibet Plateau in further.
应用数值方法模拟了飞行器升力面下表面喷气的增升作用。
The aerodynamic characteristics of an airfoil with a jet issuing from its lower surface are investigated by numerical method.
增升减阻一直是空气动力设计工作者追求的目标。
The unique aim of aerodynamic designer is always to enhance lift coefficient and reduce drag coefficient.
该文研究结果可以为大型飞机的增升装置地面效应设计提供参考依据。
The results of the simulation may provide a theoretical basis for the design of height lift devices of large aircraft in ground effect.
以典型三段翼型为对象，采用数值模拟方法，研究了在襟翼上增加微型后缘装置提高增升装置效率的可行性；
Choosing typical three element airfoil and based on numerical simulation method, the feasibility of MINI-TED to improve aerodynamic performance of high lift system is studied.
单一增大气流出口压力时增升效果无明显变化。
The lift does not depend on the variation of jet pressure closely.
研究表明：微型后缘装置明显改变了襟翼后缘弯度，对襟翼流动产生有利诱导作用，拓展加长了增升装置的有效“气动弦长”，是一种附加“气动襟翼”。
The study shows that: Mini-TED changes the curvature of trailing edge and increases effective aerodynamic chord length for high lift system, is an additional 'aerodynamic flap'.
研究表明：微型后缘装置明显改变了襟翼后缘弯度，对襟翼流动产生有利诱导作用，拓展加长了增升装置的有效“气动弦长”，是一种附加“气动襟翼”。
The study shows that: Mini-TED changes the curvature of trailing edge and increases effective aerodynamic chord length for high lift system, is an additional 'aerodynamic flap'.
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