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相关概念视频

Lift01:23

Lift

125
Lift is a fundamental aerodynamic force that acts perpendicular to the direction of airflow. It plays a central role in achieving and sustaining flight and in stabilizing various vehicles. Lift primarily originates from pressure differences created across surfaces, such as an airfoil. A lower pressure region forms above the wing, while a higher pressure region forms below it, generating an upward force. This differential results from the shape and orientation of the airfoil, enabling the wing...
125
Bending of Members Made of Several Materials01:08

Bending of Members Made of Several Materials

152
In analyzing a structural member composed of two different materials with identical cross-sectional areas, it is crucial to understand how their distinct elastic properties affect the member's response under load. The analysis involves assessing stress and strain distributions using the transformed section concept, which accounts for variations in material properties.
Hooke's Law determines stress in each material, stating that stress is proportional to strain but varies due to each...
152
Stress Concentrations in Circular Shafts01:18

Stress Concentrations in Circular Shafts

176
Consider the elastic torsion formula, which applies to a circular shaft with a consistent cross-section. This formula assumes that the shaft's ends are loaded with rigid plates firmly attached. However, in many cases, torques are applied to the shaft through mechanisms like flange couplings or gears, which are connected by keys inserted into keyways. This application method modifies the stress distribution near the point of torque application, causing it to deviate from the distributions...
176
Eccentric Axial Loading in a Plane of Symmetry01:16

Eccentric Axial Loading in a Plane of Symmetry

196
Eccentric axial loading occurs when an axial load is applied away from the centroidal axis of a structural member. This scenario is common in engineering, where structural elements may not be directly aligned due to various design or functional requirements.
196
General External Flow Characteristics01:26

General External Flow Characteristics

164
The study of external flow is essential for creating structures and objects that interact efficiently and safely with moving fluids, such as air or water. When a body is immersed in a flowing fluid, it experiences two primary forces: drag, which opposes motion along the flow direction, and lift, which acts perpendicular to the flow. The shape, size, and orientation of the object influence these forces.Streamlined and Blunt Bodies in External FlowObjects in fluid flow are classified as...
164
Yield Criteria for Ductile Materials under Plane Stress01:25

Yield Criteria for Ductile Materials under Plane Stress

163
In designing structural elements and machine parts using ductile materials, it is crucial to ensure that these components withstand applied stresses without yielding. Yielding is initially determined through a tensile test, which evaluates the material's response to uniaxial stress. However, tensile stress is insufficient when components face biaxial or plane stress conditions This condition requires advanced criteria to predict failure.
The Maximum Shearing Stress Criterion, also known as...
163

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Structural Design and Manufacturing of a Cruiser Class Solar Vehicle
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航空弹性定制用于航空航天应用.

Junaid Najmi1, Haris Ali Khan1, Syed Saad Javaid1

  • 1Department of Aerospace Engineering, College of Aeronautical Engineering, National University of Sciences and Technology (NUST), Pakistan.

Heliyon
|January 31, 2024
PubMed
概括

使用先进复合材料的空气弹性定制通过优化飞减轻和控制来彻底改变航空航天设计. 本综述巩固了最近的进展,并确定了被动气弹性控制的未来研究方向.

关键词:
航空弹性优化优化气弹性定制是指空气弹性定制航空弹性 航空弹性航空航天应用.缓解浮动的缓解方法被动的空气弹性控制.

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科学领域:

  • 航空航天工程 航空航天工程
  • 材料科学 材料科学 材料科学
  • 结构动力学 结构动力学

背景情况:

  • 航空弹性定制对于先进的航空航天设计至关重要.
  • 快速的进步需要定期的研究整合.
  • 这项研究回顾了历史和最近的发展.

研究的目的:

  • 巩固航空弹性定制方面的最先进的研究.
  • 为新研究人员提供全面的概述.
  • 确定未来的研究方向和挑战.

主要方法:

  • 关于开创性作品和最近文学作品的评论.
  • 对研究贡献的批判性评价.
  • 关注材料,结构和优化技术的进步.

主要成果:

  • 强调了航空弹性定制的先进复合材料的最新发展.
  • 识别了新的优化技术和材料/结构技术.
  • 强调减轻飞和被动气弹性控制.

结论:

  • 航空弹性定制为航空航天应用提供了巨大的潜力.
  • 在优化,验证和工业采用方面仍然存在挑战.
  • 未来的研究应该专注于新材料,优化方法,并解决实际实施的障碍.