propeller area ratio

简明释义

螺旋桨盘面比

英英释义

The propeller area ratio is the ratio of the total blade area of a propeller to the area of the circle described by the tips of the blades when the propeller is rotating, indicating the efficiency of the propeller in generating thrust.

螺旋桨面积比是指螺旋桨总叶片面积与螺旋桨旋转时叶片尖端所描绘的圆形面积的比值,表明螺旋桨在产生推力方面的效率。

例句

1.Adjusting the propeller area ratio can enhance the maneuverability of the vessel.

调整螺旋桨面积比可以增强船舶的机动性。

2.The design of the ship's propeller must consider the propeller area ratio for optimal fuel efficiency.

船舶螺旋桨的设计必须考虑螺旋桨面积比以实现最佳燃油效率。

3.The efficiency of a marine vessel can be significantly improved by optimizing the propeller area ratio.

通过优化螺旋桨面积比,可以显著提高海洋船舶的效率。

4.A larger propeller area ratio can lead to better performance in low-speed applications.

较大的螺旋桨面积比可以在低速应用中带来更好的性能。

5.Engineers often analyze the propeller area ratio to ensure maximum thrust and minimal drag.

工程师们常常分析螺旋桨面积比以确保最大推力和最小阻力。

作文

The field of aerodynamics is a complex and fascinating area of study that involves understanding how air interacts with solid objects, particularly those designed for flight. One critical concept within this field is the propeller area ratio, which plays a significant role in determining the efficiency and performance of propellers used in various types of aircraft. The propeller area ratio (推进器面积比) is defined as the ratio of the total area of the propeller blades to the area of the circle described by the propeller's rotation. This ratio is essential for engineers and designers when optimizing propeller design for specific aircraft applications.Understanding the propeller area ratio is vital for several reasons. First, it directly influences the thrust produced by the propeller. A higher propeller area ratio typically indicates a larger blade area relative to the disk area, which can result in increased thrust at lower speeds. This characteristic is particularly advantageous for aircraft that require high lift during takeoff and landing phases. Conversely, a lower propeller area ratio may be more efficient at higher speeds, where drag becomes a critical factor.Moreover, the propeller area ratio also affects the overall aerodynamic efficiency of the aircraft. When designing a propeller, engineers must balance the need for thrust with the desire to minimize drag. An optimal propeller area ratio helps achieve this balance, ensuring that the propeller can operate efficiently across a range of speeds and conditions. For example, a well-designed propeller with an appropriate propeller area ratio can significantly enhance fuel efficiency, which is crucial in today's aviation industry where reducing operational costs and environmental impact is a priority.Another important aspect of the propeller area ratio is its influence on noise levels generated by the propeller. Propeller noise is a significant concern, especially in urban areas where aircraft operate close to populated regions. By carefully selecting the propeller area ratio, designers can help mitigate noise pollution while still providing the necessary thrust and performance. This consideration is increasingly important as regulatory standards for noise emissions become more stringent.In conclusion, the propeller area ratio is a fundamental concept in the design and performance of aircraft propellers. It impacts thrust generation, aerodynamic efficiency, and noise production, making it a crucial factor for engineers to consider during the design process. As technology advances and the demand for more efficient and quieter aircraft grows, understanding and optimizing the propeller area ratio will remain a key focus in the aerospace industry. By mastering this concept, future engineers can contribute to the development of innovative solutions that enhance aircraft performance while addressing environmental concerns.

在空气动力学领域,理解空气如何与固体物体相互作用,尤其是那些设计用于飞行的物体,是一个复杂而迷人的研究领域。其中一个关键概念是推进器面积比,它在确定各种类型飞机中使用的推进器的效率和性能方面起着重要作用。推进器面积比propeller area ratio)被定义为推进器叶片的总面积与推进器旋转所描述的圆的面积之间的比率。这个比率对于工程师和设计师在优化特定飞机应用的推进器设计时至关重要。理解推进器面积比非常重要,原因有几个。首先,它直接影响推进器产生的推力。较高的推进器面积比通常表明相对于盘面面积,叶片面积较大,这可以在较低速度下产生更大的推力。这一特性对于需要在起飞和着陆阶段提供高升力的飞机尤其有利。相反,较低的推进器面积比可能在较高速度下更有效,此时阻力成为关键因素。此外,推进器面积比还会影响飞机的整体空气动力学效率。在设计推进器时,工程师必须平衡推力需求与减少阻力的愿望。最佳的推进器面积比有助于实现这种平衡,确保推进器能够在各种速度和条件下高效运行。例如,设计良好的、具有适当推进器面积比的推进器可以显著提高燃油效率,这在当今航空业中至关重要,因为降低运营成本和环境影响是优先事项。推进器面积比的另一个重要方面是其对推进器产生的噪音水平的影响。推进器噪音是一个重大问题,特别是在飞机在靠近人口稠密地区的城市区域操作时。通过仔细选择推进器面积比,设计师可以帮助减轻噪音污染,同时仍提供必要的推力和性能。随着噪音排放的监管标准日益严格,这一考虑变得越来越重要。总之,推进器面积比是飞机推进器设计和性能中的基本概念。它影响推力生成、空气动力学效率和噪音产生,使其成为工程师在设计过程中必须考虑的关键因素。随着技术的进步和对更高效、更安静飞机的需求不断增长,理解和优化推进器面积比将始终是航空航天工业的关注重点。通过掌握这一概念,未来的工程师可以为开发创新解决方案做出贡献,从而提高飞机性能,同时应对环境问题。

相关单词

propeller

propeller详解:怎么读、什么意思、用法

ratio

ratio详解:怎么读、什么意思、用法