oblique shock wave

简明释义

斜冲花

英英释义

An oblique shock wave is a type of shock wave that occurs at an angle to the direction of flow, typically in supersonic flows, causing a sudden change in pressure, temperature, and density of the fluid.

倾斜激波是一种发生在流动方向角度上的激波,通常出现在超音速流动中,导致流体的压力、温度和密度发生突然变化。

例句

1.The formation of an oblique shock wave can significantly alter the flow characteristics around a wing.

一个倾斜激波的形成可以显著改变机翼周围的流动特性。

2.Engineers must consider the effects of oblique shock waves when designing high-speed vehicles.

工程师在设计高速车辆时必须考虑倾斜激波的影响。

3.The study of oblique shock waves is crucial for understanding supersonic aerodynamics.

研究倾斜激波对于理解超音速空气动力学至关重要。

4.The aircraft experienced an oblique shock wave during its supersonic flight, which caused a sudden change in pressure.

飞机在超音速飞行中经历了一个倾斜激波,导致压力突然变化。

5.In wind tunnel tests, we observed how oblique shock waves interact with boundary layers.

在风洞测试中,我们观察到了倾斜激波与边界层的相互作用。

作文

In the field of fluid dynamics and aerodynamics, understanding various types of shock waves is crucial for engineers and scientists. One significant type of shock wave is the oblique shock wave, which occurs when a supersonic flow encounters a surface at an angle. This phenomenon is particularly important in the design of high-speed aircraft and missiles, where maintaining control and stability is essential. An oblique shock wave forms when the flow direction changes due to the presence of a wedge or an angled surface. As the supersonic flow interacts with this surface, it compresses and accelerates, resulting in a sudden increase in pressure and temperature. Unlike normal shock waves, which occur perpendicular to the flow, oblique shock waves allow for a smoother transition in the flow direction, leading to less drag and maintaining higher speeds. The mathematical modeling of oblique shock waves involves the use of the conservation laws of mass, momentum, and energy. Engineers utilize these principles to predict the behavior of airflow over wings and fuselages at high speeds. The angle of the oblique shock wave can be calculated using the Mach number of the incoming flow and the geometry of the surface. This relationship is critical for optimizing the design of supersonic vehicles, ensuring that they can achieve their desired performance without experiencing excessive drag or structural failure. In practical applications, the effects of oblique shock waves are observed in various scenarios, such as during takeoff and landing of supersonic jets, or when missiles travel through the atmosphere. The design of these vehicles must account for the changes in pressure and temperature caused by oblique shock waves to ensure safety and efficiency. Engineers often conduct wind tunnel tests to visualize and measure the impact of these shock waves on model aircraft, allowing them to refine their designs before actual production. Furthermore, understanding oblique shock waves extends beyond aviation. In astrophysics, similar principles apply when studying shock waves produced by supernovae or the interaction of stellar winds with surrounding materials. The study of oblique shock waves in these contexts helps scientists gain insights into the dynamics of cosmic phenomena and the evolution of galaxies. In conclusion, the concept of oblique shock waves is fundamental in both theoretical and practical aspects of fluid dynamics. Their unique characteristics distinguish them from other types of shock waves, making them essential for the advancement of high-speed technology. As research continues to evolve, a deeper understanding of oblique shock waves will undoubtedly lead to innovations that push the boundaries of what is possible in aerodynamics and beyond.

在流体动力学和空气动力学领域,理解各种类型的冲击波对工程师和科学家至关重要。其中一个重要的冲击波类型是斜冲击波,它发生在超音速流动以一定角度遇到表面时。这种现象在高速飞机和导弹的设计中尤为重要,因为保持控制和稳定性是必不可少的。 当超音速流动与楔形或倾斜表面相互作用时,就会形成斜冲击波。随着超音速流动与该表面的相互作用,它被压缩并加速,导致压力和温度的突然增加。与垂直于流动的正常冲击波不同,斜冲击波允许流动方向的平滑过渡,从而减少阻力并保持更高的速度。 对斜冲击波的数学建模涉及质量、动量和能量的守恒定律。工程师利用这些原理来预测超音速飞行器的气流行为。斜冲击波的角度可以通过来流的马赫数和表面的几何形状进行计算。这一关系对于优化超音速飞行器的设计至关重要,确保它们能够实现预期的性能,而不会遭受过大的阻力或结构失效。 在实际应用中,斜冲击波的影响在各种场景中都有所体现,例如超音速喷气式飞机的起飞和着陆,或导弹穿越大气层时。设计这些飞行器时必须考虑到斜冲击波引起的压力和温度变化,以确保安全和效率。工程师们通常进行风洞测试,以可视化和测量这些冲击波对模型飞机的影响,从而在实际生产之前完善他们的设计。 此外,理解斜冲击波的概念不仅限于航空。在天体物理学中,当研究超新星产生的冲击波或恒星风与周围物质的相互作用时,类似的原理也适用。研究这些背景下的斜冲击波有助于科学家深入了解宇宙现象的动力学和星系的演化。 总之,斜冲击波的概念在流体动力学的理论和实践方面都是基础。它们独特的特性使其与其他类型的冲击波区分开来,使其成为高速度技术进步的关键。随着研究的不断发展,对斜冲击波的更深入理解无疑将导致推动空气动力学及其他领域的创新。