Institution
Pratt & Whitney
About: Pratt & Whitney is a based out in . It is known for research contribution in the topics: Turbine & Turbine blade. The organization has 3018 authors who have published 3219 publications receiving 55432 citations.
Topics: Turbine, Turbine blade, Combustor, Propulsion, Combustion chamber
Papers published on a yearly basis
Papers
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01 Jan 1977826 citations
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777 citations
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TL;DR: In this article, a comparison is made for a 15-run Box-Behnken design using both the intended design settings and the actual design settings, and cutoff values are suggested for use to determine when an effect's variance inflation factor is too large to keep that effect in the model.
Abstract: When creating designed experiments, it is not always possible to run the experiment at the exact settings required to maintain orthogonal effects. However, this is not measurement error when precise measurements of the settings can be made once the experiment begins. A comparison is made for a 15-run Box–Behnken design using both the intended design settings and the actual design settings. Variance inflation factors are used to measure the induced collinearity in the effects. Two cutoff values are suggested for use to determine when an effect's variance inflation factor is too large to keep that effect in the model.
776 citations
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604 citations
01 Mar 2014
TL;DR: In this article, the results of a study to address the long range, strategic planning required by NASA's Revolutionary Computational Aerosciences (RCA) program in the area of computational fluid dynamics (CFD), including future software and hardware requirements for High Performance Computing (HPC), are presented.
Abstract: This report documents the results of a study to address the long range, strategic planning required by NASA's Revolutionary Computational Aerosciences (RCA) program in the area of computational fluid dynamics (CFD), including future software and hardware requirements for High Performance Computing (HPC). Specifically, the "Vision 2030" CFD study is to provide a knowledge-based forecast of the future computational capabilities required for turbulent, transitional, and reacting flow simulations across a broad Mach number regime, and to lay the foundation for the development of a future framework and/or environment where physics-based, accurate predictions of complex turbulent flows, including flow separation, can be accomplished routinely and efficiently in cooperation with other physics-based simulations to enable multi-physics analysis and design. Specific technical requirements from the aerospace industrial and scientific communities were obtained to determine critical capability gaps, anticipated technical challenges, and impediments to achieving the target CFD capability in 2030. A preliminary development plan and roadmap were created to help focus investments in technology development to help achieve the CFD vision in 2030.
489 citations
Authors
Showing all 3018 results
Name | H-index | Papers | Citations |
---|---|---|---|
Anthony G. Evans | 130 | 576 | 65803 |
Edward M. Greitzer | 50 | 152 | 9385 |
Ranjan Ganguli | 43 | 324 | 5900 |
Isaac F. Silvera | 41 | 255 | 7368 |
Gabriel L. Suciu | 33 | 398 | 4154 |
Thomas A. Cruse | 29 | 84 | 3790 |
Robert F. Kunz | 28 | 119 | 3102 |
James E. Harvey | 27 | 154 | 2653 |
M.L. Emiliani | 27 | 37 | 2445 |
Christopher M. Dye | 25 | 87 | 1549 |
Michael L. Perry | 25 | 107 | 3719 |
Stephen M. Copley | 23 | 67 | 1936 |
Allan J. Volponi | 21 | 52 | 1523 |
Greg Foliente | 21 | 65 | 1640 |
Daniel J. Dorney | 20 | 118 | 1344 |