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Related Concept Videos

Composite Bodies00:55

Composite Bodies

A composite body is a body made up of multiple parts, connected to form a larger, unified object. Each part has its own weight and center of gravity, which must be considered to determine the center of gravity of the composite body. In cases where the density or specific weight is constant, the center of gravity coincides with the centroid.
Composite bodies have widespread applications in mechanical engineering, from automobiles to aircraft to rockets. For example, an automobile wheel comprises...
Unsymmetric Loading of Thin-Walled Members: Problem Solving01:07

Unsymmetric Loading of Thin-Walled Members: Problem Solving

The shear center of a channel section with uniform thickness, height, and width, is determined by computing the shear force in the member and calculating the moments of inertia of the sections.
To compute the shear forces, find the shear flow at a specific distance from the endpoint using the vertical shear and the moment of inertia values. The total shear force on the flange is calculated by integrating the shear flow from one end of the flange to the other.
Next, calculate the moments of...
Unsymmetric Loading of Thin-Walled Members01:23

Unsymmetric Loading of Thin-Walled Members

Thin-walled members with non-symmetrical cross-sections are vital to engineering structures, offering material efficiency and structural integrity. However, unsymmetrical loading on these members leads to complex stress distributions, resulting in simultaneous bending and twisting can cause deformation or structural failure. The interaction between bending and twisting requires detailed analysis to ensure structural resilience.
The concept of the shear center is crucial in countering the...
Design of Prismatic Beams for Bending01:23

Design of Prismatic Beams for Bending

The design of prismatic beams, structural elements with a uniform cross-section, focuses on ensuring safety and structural integrity under load. The design process begins by determining the allowable stress, either from material properties tables, or by dividing the material's ultimate strength by a safety factor. This safety factor is essential for accommodating uncertainties, and varies depending on the material—timber, steel, or concrete—with each having unique strength and stress...
Internal Loadings in Structural Members: Problem Solving01:28

Internal Loadings in Structural Members: Problem Solving

When designing or analyzing a structural member, it is important to consider the internal loadings developed within the member. These internal loadings include normal force, shear force, and bending moment. Engineers can ensure that the structural member can support the applied external forces by calculating these internal loadings.
To illustrate this, let's consider a beam OC of 5 kN, inclined at an angle of 53.13° with the horizontal and supported at both ends. Determine the internal loadings...
Bending of Members Made of Several Materials01:11

Bending of Members Made of Several Materials

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 material's...

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Related Experiment Video

Updated: Jun 13, 2026

Knowledge Based Cloud FE Simulation of Sheet Metal Forming Processes
11:05

Knowledge Based Cloud FE Simulation of Sheet Metal Forming Processes

Published on: December 13, 2016

Lightweight Structural Design of UAM Fuselage Using AI Predictive Modeling and Composite Big Data from Automated

Woo Hyuk Son1,2, Ji Hoon Kim2, Sung-Youl Bae1

  • 1Aerospace Defense Research Group, Korea Institute of Ceramic Engineering & Technology, 101 Soho-ro, Jinju 52851, Republic of Korea.

Materials (Basel, Switzerland)
|June 12, 2026
PubMed
Summary
This summary is machine-generated.

This study introduces an AI-driven method for designing lightweight, structurally sound airframes for urban air mobility (UAM). Composite materials significantly reduce weight by up to 50% while maintaining structural integrity for electric aircraft.

Keywords:
data-driven predictive modeldesign processfiber reinforcement plastics (FRP)structural analysisurban air mobility (UAM)

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Last Updated: Jun 13, 2026

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Area of Science:

  • Materials Science
  • Aerospace Engineering
  • Artificial Intelligence

Background:

  • Rapid urbanization causes traffic congestion and air pollution, increasing the need for sustainable transport solutions like urban air mobility (UAM).
  • Lightweight yet structurally robust airframes are crucial for the commercial viability of electric propulsion-based UAM systems.
  • Current design processes often lack efficiency in optimizing composite material properties for advanced aerospace applications.

Purpose of the Study:

  • To develop an optimized lightweight airframe design process for UAM.
  • To integrate automated composite manufacturing with AI-based material property prediction.
  • To demonstrate the effectiveness of AI in predicting mechanical properties for novel composite materials.

Main Methods:

  • Finite-element analysis (FEA) was used to determine material properties (elastic modulus, weight reduction) of fiber-reinforced polymers (glass, basalt, carbon).
  • An automated manufacturing process generated a large dataset of fiber-reinforced plastics.
  • A deep learning regression model was developed using Altair AI Studio to predict mechanical properties.

Main Results:

  • FEA on a UAM fuselage model using predicted composite properties showed up to 50% weight reduction compared to aluminum with equivalent or superior stiffness.
  • Inverse reserve factor (IRF) analysis confirmed structural safety, with all configurations having IRF values below 1.
  • The AI-driven framework successfully predicted mechanical properties for untested material and process conditions.

Conclusions:

  • The proposed AI-driven framework offers a scalable, data-driven methodology for lightweight composite airframe design.
  • This approach is applicable to next-generation UAM and advanced air mobility structures.
  • The study validates the use of AI in accelerating the development of efficient and safe aerospace designs.