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Model Verification and Validation Concepts for a Probabilistic Fracture Assessment Model to Predict Cracking of Knife Edge Seals in the Space Shuttle Main Engine High Pressure Oxidizer

机译:概率断裂评估模型的模型验证和验证概念,用于预测航天飞机主机高压氧化剂中的刀口密封件破裂

摘要

Physics-based models are routinely used to predict the performance of engineered systems to make decisions such as when to retire system components, how to extend the life of an aging system, or if a new design will be safe or available. Model verification and validation (V&V) is a process to establish credibility in model predictions. Ideally, carefully controlled validation experiments will be designed and performed to validate models or submodels. In reality, time and cost constraints limit experiments and even model development. This paper describes elements of model V&V during the development and application of a probabilistic fracture assessment model to predict cracking in space shuttle main engine high-pressure oxidizer turbopump knife-edge seals. The objective of this effort was to assess the probability of initiating and growing a crack to a specified failure length in specific flight units for different usage and inspection scenarios. The probabilistic fracture assessment model developed in this investigation combined a series of submodels describing the usage, temperature history, flutter tendencies, tooth stresses and numbers of cycles, fatigue cracking, nondestructive inspection, and finally the probability of failure. The analysis accounted for unit-to-unit variations in temperature, flutter limit state, flutter stress magnitude, and fatigue life properties. The investigation focused on the calculation of relative risk rather than absolute risk between the usage scenarios. Verification predictions were first performed for three units with known usage and cracking histories to establish credibility in the model predictions. Then, numerous predictions were performed for an assortment of operating units that had flown recently or that were projected for future flights. Calculations were performed using two NASA-developed software tools: NESSUS(Registered Trademark) for the probabilistic analysis, and NASGRO(Registered Trademark) for the fracture mechanics analysis. The goal of these predictions was to provide additional information to guide decisions on the potential of reusing existing and installed units prior to the new design certification.
机译:基于物理的模型通常用于预测工程系统的性能,以做出决策,例如何时停用系统组件,如何延长老化系统的寿命,或者新设计是否安全或可用。模型验证和确认(V&V)是在模型预测中建立信誉的过程。理想情况下,将设计并执行精心控制的验证实验以验证模型或子模型。实际上,时间和成本约束限制了实验乃至模型开发。本文介绍了在概率断裂评估模型的开发和应用过程中模型V&V的要素,该模型可以预测航天飞机主机高压氧化剂涡轮泵刀口密封件中的裂纹。这项工作的目的是评估在不同的使用和检查情况下,在特定的飞行单元中引发裂纹并将裂纹扩展到指定破坏长度的可能性。在这项研究中开发的概率性骨折评估模型结合了一系列子模型,这些子模型描述了用法,温度历史,颤动趋势,牙齿应力和周期数,疲劳裂纹,无损检查以及最终的故障概率。该分析考虑了温度,颤振极限状态,颤振应力大小和疲劳寿命属性之间的单位变化。调查重点是计算使用场景之间的相对风险,而不是绝对风险。首先对三个具有已知用法和破解历史记录的单元进行验证预测,以建立模型预测的可信度。然后,对最近飞行的或预计用于未来飞行的各种作战单位进行了许多预测。使用两个NASA开发的软件工具进行计算:用于概率分析的NESSUS(注册商标)和用于断裂力学分析的NASGRO(注册商标)。这些预测的目的是提供更多信息,以指导有关在获得新设计认证之前重用现有和已安装单元的潜力的决策。

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