By David M. Schuster (auth.), Alexander Kuzmin (eds.)
The overseas convention on Computational Fluid Dynamics is held each years and brings jointly physicists, mathematicians and engineers to check and percentage fresh advances in mathematical and computational strategies for modeling fluid move. The court cases of the 2010 convention (ICCFD6) held in St Petersburg, Russia, include a variety of refereed contributions and are supposed to function a resource of reference for all these drawn to the state-of-the-art in computational fluid dynamics.
Read or Download Computational Fluid Dynamics 2010: Proceedings of the Sixth International Conference on Computational Fluid Dynamics, ICCFD6, St Petersburg, Russia, on July 12-16, 2010 PDF
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Extra info for Computational Fluid Dynamics 2010: Proceedings of the Sixth International Conference on Computational Fluid Dynamics, ICCFD6, St Petersburg, Russia, on July 12-16, 2010
1 Introduction Traditionally, Computational Fluid Dynamics (CFD) methods developers have applied a very logical, systematic approach to software development, termed here as the “Develop, Validate, Apply” strategy. In this strategy, “Develop” refers to the coding and verification of the CFD software, while “Validate” refers to the process of running test cases on the software and comparing with known data. These validation data sources can be from other validated CFD methods, sub-scale experiments such as wind tunnel tests, or in rare cases, full-scale data, such as that obtained from flight tests.
This high-risk EVA underscored the importance of accurate analysis capability to future missions and the impact it could Fig. 3 Space Shuttle performing flip maneuver as it approaches the International Space Station Expanding Role of Applications in the Development and Validation of CFD at NASA 9 Fig. 4 Removal of protruding heatshield gap filler during STS-114 mission have on the risk posture of these missions. The gap filler analysis was also a harbinger of how our analysis techniques would be stressed and extended during future flights.
In partial response to the accident and the findings of the investigation, NASA established a new organization known as the NASA Engineering and Safety Center (NESC). The NESC operates under the philosophy of three primary tenets to ensure safety: (1) Strong in-line technical checks and balances to ensure proper engineering analysis and data are being applied to the problem. (2) Healthy tension between the Project, Safety, and Engineering components supporting the Program. (3) “Value added” independent assessment of problems that cannot be adequately resolved within the internal Program environment.
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