用虚拟测试和混合仿真打破测试金字塔

Q4 Engineering Fatigue of Aircraft Structures Pub Date : 2019-12-01 DOI:10.2478/fas-2019-0001
S. You, X. Shawn Gao, A. Nelson
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引用次数: 4

摘要

摘要虚拟测试和混合仿真已经成为飞机设计和验证的一个重要趋势。强调单轴试件试验和全结构认证试验的传统金字塔(或积木)试验方法正受到挑战。研究人员正试图使用先进的测试和模拟方法来取代金字塔测试方法。在物理测试之前,可以进行虚拟测试来模拟物理测试。可以构建和验证包括控制器、执行器和夹具在内的完整测试系统的虚拟模型。在这项工作中,开发并验证了一个示例,以显示虚拟测试过程的潜力。混合仿真是一种在实际载荷条件下分析分析模型和物理结构集成系统的方法。混合模拟将实验室测试与数值分析相结合,以探索这两种方法的优点。在这项研究中,对一个简化的机翼进行了混合模拟,以证明这一过程。虚拟测试和混合模拟是测试金字塔方法的替代方法。认证仍然需要进行全尺寸测试,但对供试品的了解越多,在全尺寸认证测试中成功的机会就越大。
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Breaking the Testing Pyramid with Virtual Testing and Hybrid Simulation
Abstract Virtual testing and hybrid simulation have become an important trend in airplane design and validation. The traditional Testing Pyramid (or Building Block) approaches that emphasis on uniaxial coupon test and full structure certification test are being challenged. Researchers are trying to use advanced testing and simulation methods to replace the Testing Pyramid approach. Before physical testing, virtual testing can be conducted to simulate the physical test. Virtual model of the full testing system including controller, actuators, and fixtures can be constructed and validated. In this work, an example has been developed and validated to show the potentials of the virtual testing process. Hybrid simulation is an approach of analyzing an analysis model and physical structure integrated system under realistic loading conditions. Hybrid simulation combines the lab testing with numerical analysis to explore the benefits of both methodologies. In this study, a hybrid simulation for a simplified airplane wing was conducted to demonstrate the process. Virtual testing and hybrid simulation are alternative methods of Testing Pyramid approach. Full scale tests are still required for certification but the more that is known about the test article, the greater chances of success in the full-scale certification testing.
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来源期刊
Fatigue of Aircraft Structures
Fatigue of Aircraft Structures Engineering-Safety, Risk, Reliability and Quality
CiteScore
0.40
自引率
0.00%
发文量
0
期刊介绍: The publication focuses on problems of aeronautical fatigue and structural integrity. The preferred topics include: full-scale fatigue testing of aircraft and aircraft structural components, fatigue of materials and structures, advanced materials and innovative structural concepts, damage tolerant design of aircraft structure, life extension and management of ageing fleets, structural health monitoring and loads, fatigue crack growth and life prediction methods, NDT inspections, airworthiness considerations.
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