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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.


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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

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

NameH-indexPapersCitations
Anthony G. Evans13057665803
Edward M. Greitzer501529385
Ranjan Ganguli433245900
Isaac F. Silvera412557368
Gabriel L. Suciu333984154
Thomas A. Cruse29843790
Robert F. Kunz281193102
James E. Harvey271542653
M.L. Emiliani27372445
Christopher M. Dye25871549
Michael L. Perry251073719
Stephen M. Copley23671936
Allan J. Volponi21521523
Greg Foliente21651640
Daniel J. Dorney201181344
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Performance
Metrics
No. of papers from the Institution in previous years
YearPapers
202123
202043
201933
201845
201745
201642