File:Aerodynamic design using parallel processors (IA aerodynamicdesig1094539914).pdf
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Summary[edit]
Aerodynamic design using parallel processors
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| Author |
Brawley, Stephen C. |
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| Title |
Aerodynamic design using parallel processors |
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| Publisher |
Monterey, California. Naval Postgraduate School |
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| Description |
An airfoil design technique has been developed which decreases the computational processing time by more than an order of magnitude when optimizing aerodynamic performance. The practicality of airfoil design using parallel processors and Navier-Stokes flow solvers has been demonstrated. Typically, an airfoil is designed to meet certain criteria based upon its aerodynamic performance at set flight conditions. If an optimization technique is used for airfoil design, the shape of the airfoil is varied, and the aerodynamic performance of numerous airfoil geometries are evaluated using computational fluid dynamics. Multiple aerodynamic performance evaluations require the vast majority of computational processing time used in airfoil design optimization. Subjects: Aerodynamic design; Optimization; Parallel processing; Runge-Kutta Euler Solver |
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| Language | English | |
| Publication date | September 1993 | |
| Current location |
IA Collections: navalpostgraduateschoollibrary; fedlink |
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| Accession number |
aerodynamicdesig1094539914 |
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| Source | ||
| Permission (Reusing this file) |
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. As such, it is in the public domain, and under the provisions of Title 17, United States Code, Section 105, may not be copyrighted. | |
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This file is a work of a sailor or employee of the U.S. Navy, taken or made as part of that person's official duties. As a work of the U.S. federal government, it is in the public domain in the United States.
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| This file has been identified as being free of known restrictions under copyright law, including all related and neighboring rights. | ||
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| current | 01:18, 14 July 2020 |  | 1,275 × 1,650, 153 pages (4.39 MB) | Fæ (talk | contribs) | FEDLINK - United States Federal Collection aerodynamicdesig1094539914 (User talk:Fæ/IA books#Fork8) (batch 1993-2020 #5655) |
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