首页> 外文会议>AIAA aerodynamic decelerator systems technology conference and seminar >The Road Ahead: A White Paper on the Development, Testing and Use of Advanced Numerical Modeling for Aerodynamic Decelerator Systems Design and Analysis By the AIAA-ADS sub-committee on Advanced Modeling Development and Validation
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The Road Ahead: A White Paper on the Development, Testing and Use of Advanced Numerical Modeling for Aerodynamic Decelerator Systems Design and Analysis By the AIAA-ADS sub-committee on Advanced Modeling Development and Validation

机译:领先的道路:白皮书有关AIAA-ADS小组委员会高级建模和验证的AIAA-ADS分组设计和分析先进数值模型的开发,测试和使用的白皮书

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Quantitative engineering analysis of parachutes and inflatables has been part of the routine design process since the days of World War II. But in most cases, the shear complexity in which their flexible structure interact both externally and internally with the surrounding air demands that empirical data be used to either validate or supplement such analysis. Advanced modeling embodied in the techniques of Computational Fluid Dynamics (CFD), Computational Structure Dynamics (CSD) and Fluid-Structure Interactions (FSI) has great potential for diminishing such reliance. But even though its application to aerodynamic decelerator systems (ADS) has been under consideration for the past four decades, progress has been painfully slow and the results rarely integrated into today's engineering design practice. This report aims at discussing why advanced modeling has not reached the level of practical use that has occurred in other aerospace fields. Such lack of progress origins partly from advanced modeling requiring substantial human resources that are not usually associated with parachute programs (expertise in computational methods in particular). Moreover, the extensive experimental database for Verification and Validation needed to support advanced modeling development is missing. This white paper begins with a pedagogical review of the most current implementations of CFD, CSD and/or FSI in the context of ADS applications. This is followed by a discussion of both non-ADS and ADS examples in which advanced modeling has been shown to yield interesting and relevant results. The report also identifies the type of data and measurement techniques that are needed for V&V, as well as the most pressing challenges - both theoretical and empirical - that are impeding progress. The paper ends with a series of recommendations for action items to be considered in the near and long terms.
机译:自第二次世界大战日以来,降落伞和充气的定量工程分析是常规设计过程的一部分。但在大多数情况下,它们的柔性结构在外部和内部与周围空气相互作用的剪切复杂性要求经验数据用于验证或补充这种分析。在计算流体动力学(CFD),计算结构动态(CSD)和流体结构相互作用(FSI)中体现的高级建模具有巨大的依赖性递减的潜力。但即使在过去的四十年中已经考虑到空气动力学减速器系统(广告)的应用,即使在过去的四十年中已经考虑,进展令人痛苦缓慢,结果很少集成到今天的工程设计实践中。本报告旨在讨论为什么先进的建模尚未达到其他航空航天领域发生的实际使用水平。这种缺乏进展起源于需要大量人力资源的先进建模,这些资源通常与降落伞计划(特别是计算方法的专业知识)。此外,缺少了支持高级建模开发所需的验证和验证的广泛实验数据库。本白皮书在广告应用程序的上下文中始于对CFD,CSD和/或FSI最新实现的教学评价。随后是对非广告和广告的讨论,其中已显示高级建模,以产生有趣和相关结果。该报告还确定了V&V所需的数据和测量技术,以及最紧迫的挑战 - 都是受阻进步的理论和经验。本文以近乎长的条件考虑的行动项目为止了一系列建议。

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