在关键马赫数时,通过被动控制突然扩大的流量和沿管道的温度分布
Shahid Tamboli1, Sayed Ahmed Imran Bellary2, Roslinda Abdullah3
1Symbiosis Institute of Technology, Symbiosis International University, Pune, Maharashtra, India.
Scientific reports
|January 7, 2026
概括
在航空航天应用中,四分之一的肋骨有效地控制了马赫1.0的基压. 这些肋骨的最佳位置和尺寸可以最大限度地减少阻力,并通过管理循环区来提高燃料效率.
科学领域:
- 航空航天工程 航空航天工程
- 流体动力学 流体动力学
- 声学 声学 在声学方面
背景情况:
- 航空航天领域的粗基通常会经历突如其来的缓解增加,导致循环回收区减少压力并增加阻力.
- 控制基压对于提高空气动力学性能和系统效率至关重要.
研究的目的:
- 为了研究使用四分之一的肋骨控制轴对称管道的底压在马赫1.0.0.的使用.
- 为了确定最优的肋骨大小,位置和喷嘴压力比率 (NPR) 来操纵基压.
主要方法:
- 使用ANSYS Fluent进行计算流体动力学 (CFD) 模拟.
- 研究了各种肋骨尺寸 (半径1-2.5毫米) 和位置 (0.5D-2.0D) 在不同长度的管道内 (L/D = 1-6).
主要成果:
- 四分之一肋骨通过与剪切层和管道壁相互作用,显著影响底部压力,影响流量重新连接.
- 与0.5D和1D相比,放置在1.5D和2D的肋骨在控制基压方面表现出更大的有效性.
- 较大的肋半径促进了剪切层的重新连接,导致基压增加.
结论:
- 四分之一肋提供了一个可行的被动控制策略,用于高速空气动力学的底压管理.
- 优化的肋骨设计和放置可以提高系统可靠性,降低成本,提高燃油效率,与环境目标保持一致.
相关概念视频
Laminar Flow: Problem Solving
500
Laminar flow occurs when a fluid moves smoothly in parallel layers with minimal mixing and turbulence. In fluid mechanics, ensuring laminar flow within a pipe is essential for precise control of flow characteristics, especially in engineering applications. The key factor in determining whether flow remains laminar is the Reynolds number, a dimensionless quantity that depends on the fluid's velocity, density, viscosity, and the pipe's diameter. A Reynolds number of 2100 or lower...
500
Conservation of Mass in Fixed, Nondeforming Control Volume
1.6K
The principle of conservation of mass is fundamental in fluid dynamics and is crucial for analyzing flow within fixed control volumes, such as pipes or ducts. This principle states that the total mass within a control volume remains constant unless altered by the inflow or outflow of mass through the control surfaces. This results in a vital relationship for steady, incompressible flow where the mass entering a system equals the mass leaving it.
In the case of a sewer pipe, which can be modeled...
In the case of a sewer pipe, which can be modeled...
1.6K
Steady Flow of a Fluid Stream
664
Consider a control volume, such as a pipe with solid boundaries, through which fluid flows and changes direction due to the impulse exerted by the resulting force from the pipe walls. In steady flow, the mass of fluid entering the control volume at a given time, t, with velocity v1, is equal to the mass leaving after infinitesimal time dt, with velocity v2.
During this process, the momentum of the fluid within the control volume remains constant over the time interval dt. By applying the...
During this process, the momentum of the fluid within the control volume remains constant over the time interval dt. By applying the...
664
Single Pipe Systems
426
In pipe flow analysis, problems are typically categorized into three types — Type I, Type II, and Type III — based on the known parameters and the desired outcome. Each type of problem addresses specific engineering requirements using fluid properties, pipe characteristics, and operational conditions.
In a Type I problem, fluid properties (density and viscosity), pipe characteristics (including diameter, length, and surface roughness), and the flow rate or average velocity are...
In a Type I problem, fluid properties (density and viscosity), pipe characteristics (including diameter, length, and surface roughness), and the flow rate or average velocity are...
426
Application of the Linear Momentum Equation
405
The application of the linear momentum equation can be used to analyze the forces needed to hold a 180-degree pipe bend in place with flowing water. In this case, water flows through the bend with a constant cross-sectional area of 0.01 square meters and a flow velocity of 15 meters per second. The pressure at the entrance is 0.2 Megapascals and the pressure at the exit is 0.16 Megapascals.
The goal is to determine the force components in the x and y directions to hold the pipe in place. Since...
The goal is to determine the force components in the x and y directions to hold the pipe in place. Since...
405
General Characteristics of Pipe Flow II
1.6K
When fluid enters a pipe, it first passes through the entrance region, where the velocity profile adjusts due to viscous effects. In this region, a boundary layer forms along the pipe walls and grows until it fully occupies the pipe's cross-section. Once the boundary layer merges, the flow becomes fully developed, with a steady velocity profile that remains consistent along the pipe's length.
The distance to reach a fully developed flow is called the entrance length and depends on the...
The distance to reach a fully developed flow is called the entrance length and depends on the...
1.6K


