Advanced ODLV Similarity Laws for Geometric Distortion in Stiffened Plates

Significance 

In aeronautics, shipbuilding, and construction, stiffened plates are essential for creating structures that are both lightweight and highly durable. These plates, which are thin metal sheets reinforced with ribs or stiffeners, are designed to handle external loads while keeping the weight to a minimum which makes them ideal for use in aircraft, ships, and other large-scale engineering projects where reducing weight is critical. Stiffened plates are especially valued for providing the necessary strength and stability without adding unnecessary mass. However, accurately predicting how these plates will perform under different types of loads is still a big challenge. Typically, engineers rely on scaled models to study the behavior of large structures including stiffened plates. Testing these scaled models is often quicker, more affordable, and easier to manage than working with full-size prototypes. But there’s a catch: scaling can lead to geometric distortion. Since it’s not always practical or cost-effective to scale the thickness of these plates in the same way as their length and width, the models sometimes don’t behave exactly like the real thing. This distortion means that the conventional scaling laws used to predict full-scale behavior often fall short when applied to stiffened plates. What further complicates things is the complex structure of stiffened plates, which are reinforced by stiffeners. These added components affect how the plates respond under impact, and the interactions between the plate and the stiffeners introduce another layer of difficulty. Much of the previous research has focused on simpler structures like beams or thin-walled plates, leaving the unique challenges of stiffened plates less explored.

To this account, a recent study published in Thin-Walled Structures, led by doctoral candidate Xinzhe Chang, along with Professors Fei Xu and Wei Feng from Northwestern Polytechnical University and Xiaocheng Li and Xiaochuan Liu from the Aircraft Strength Research Institute of China, the researchers developed new scaling laws to predict how stiffened plates respond to low-velocity impacts. These plates are commonly used in engineering fields, but scaling down their models while maintaining accuracy has been challenging due to issues like geometric distortion. The research team recognized that existing scaling methods often fall short when applied to stiffened plates, so they set out to create a more accurate approach. Using finite element software (ABAQUS), they ran simulations on both scaled and full-sized plates to understand how distortions affect key dynamic responses like displacement and impact forces. They focused on two types of distortion: “co-directional,” where both plate thickness and stiffener dimensions scale similarly, and “hetero-directional,” where these elements scale differently. For co-directional scaling, based on the ODLV (Oriented-Density-Length-Velocity) system, the researchers varied the thicknesses and dimensions of the stiffeners in several models to see how well they could mimic the behavior of full-sized plates. They applied low-velocity impacts using a rigid ball and then measured things like how much the plates displaced at the center. Their findings were promising: even with significant distortions, these scaled models predicted the full-sized behavior with less than an 11% error margin. This was a good sign that their approach could make scaled models more reliable for real-world use. The researchers then tackled hetero-directional scaling, which adds more complexity since the stiffeners and plate thickness scale differently, creating less uniform interactions between them. In this case, they altered the dimensions of the stiffeners separately from the plate thickness, simulating more realistic engineering conditions. Even with this added difficulty, their models remained accurate, with errors below 3%. To further test the robustness of their approach, the team experimented with scenarios where they couldn’t just adjust the stiffener dimensions to account for distortions. They tried changing things like material properties and the number of stiffeners on each plate. For instance, they looked at how varying the number of stiffeners or modifying the material’s yield stress affected the model’s accuracy. Despite these adjustments, the models still accurately predicted key responses, with an error margin under 10%. One particularly interesting outcome was when they applied a technique called “relative plastic capacity equivalence” to make sure that scaled models reflected the same level of plastic deformation as the full-sized plates. With this technique, they saw that the scaled models’ displacement over time closely matched that of the larger plates, even with significant geometric distortions. This approach not only tackled scaling issues but also helped maintain the structural integrity of the plates under impact, proving their new scaling laws to be highly effective.

To wrap up, the new study of this research team led by Prof. Fei Xu has the potential to change the game for engineers looking to test and analyze the behavior of stiffened plates, which are so important in fields like aerospace and shipbuilding. By creating new scaling laws that consider geometric distortions, the researchers have tackled a long-standing problem: the difficulty of accurately scaling stiffened plates, especially their thickness, while keeping predictions reliable. This development means that smaller models can be tested with much more confidence, cutting down on the need for costly, full-scale tests. For industries that depend on strong but lightweight materials, this research offers a great way to streamline design and lower costs. The impact of this study reaches beyond just stiffened plates under impact. The similarity laws proposed here could be used as a broader framework for working with all kinds of thin-walled structures that are hard to scale evenly. So, whether it’s aircraft fuselages or ship hulls—both of which often use stiffened plates—engineers now have a new tool for tackling these challenges. By improving the accuracy of scaled models, the new work can help speed up the design and testing of new materials and components, leading to safer and more efficient engineering solutions. Another interesting point is the use of relative plastic capacity equivalence. This approach lets engineers adjust the design of stiffeners while keeping the structure’s overall response intact. This is especially helpful when working with complex structures where geometric distortion can’t be avoided. With this method, there’s room for customization in high-stress environments, like those seen in space exploration or military applications, where innovative designs are key. In practical terms, the authors’ findings could help industries make smarter choices about materials and structural designs with more accurate models. Engineers can now design smaller-scale tests that reflect real-world conditions more closely, ultimately improving the safety and performance of large-scale structures. For more in-depth information, you can find all the academic papers from this research team at click here (or here). Don’t miss out on the latest advancements in the study on similarity of impact dynamics! Stay curious, keep exploring!

Advanced ODLV Similarity Laws for Geometric Distortion in Stiffened Plates - Advances in Engineering

About the author

Xinzhe Chang is currently a doctoral candidate at the School of Aeronautics, Northwestern Polytechnical University, China and also a Joint PhD Student at the Department of Aerospace Engineering, Khalifa University of Science and Technology, United Arab Emirates. He received his Bachelor degree in 2019 and Master degree in 2023, respectively, both in School of Aeronautics from Northwestern Polytechnical University. The main research interest is in similarity laws for structures under impact loading.

About the author

Fei Xu is currently a Professor in School of Aeronautics, Northwestern Polytechnical University. Currently, she is the director of Institute of Computational Mechanics and Engineering Applications. In 2020 she received the JACM Fellow Award from JACM. Professor Xu is the author of over 77 papers including publications in International Journal of Impact Engineering, Thin-walled structures, Ocean Engineering, Chinese Journal of Aeronautics and so on. Her research interests include the parallel algorithm of SPH meshless method, mechanism of water entry of structure and aircraft tire spray, impact dynamics similarity laws and so on.

About the author

Wei Feng is currently an Associate Professor in School of Aeronautics at Northwestern Polytechnical University. He received his B.S. in aircraft design and engineering (2013), M.S. degree in aircraft design (2015), and Ph.D. degree in Solid mechanics (2019) from Northwestern Polytechnical University. His research interests include composite damage and repair, environmental durability of aircraft structures.

References

Xinzhe Chang, Fei Xu, Wei Feng, Xiaocheng Li, Xiaochuan Liu, Similarity laws of geometric distortion for stiffened plate under low velocity impact loads, Thin-Walled Structures, Volume 199, 2024, 111830,

Go to Thin-Walled Structures

Shuai Wang, Fei Xu, Xiaoyu Zhang, Zhen Dai, Xiaochuan Liu, Chunyu Bai, A directional framework of similarity laws for geometrically distorted structures subjected to impact loads, International Journal of Impact Engineering, Volume 161, 2022, 104092.

Go to International Journal of Impact Engineering

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