contributor author | Roy J. Hartfield | |
contributor author | Rhonald M. Jenkins | |
contributor author | John E. Burkhalter | |
date accessioned | 2017-05-09T00:23:03Z | |
date available | 2017-05-09T00:23:03Z | |
date copyright | June, 2007 | |
date issued | 2007 | |
identifier issn | 1530-9827 | |
identifier other | JCISB6-25975#167_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/135388 | |
description abstract | A methodology for developing optimized designs for symmetric-centerbody ramjet powered missiles, using a genetic algorithm as the driver for the system optimization process, has been developed. The methodology described in this paper allows for a comprehensive but efficient exploration of the design space. This global optimization process is made possible by performance prediction codes, which can provide preliminary design-level accuracy very efficiently. This work demonstrates the first truly comprehensive design strategy for this type of device. The paper contains a discussion of the methodology and shows results for a typical design scenario. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Ramjet Powered Missile Design Using a Genetic Algorithm | |
type | Journal Paper | |
journal volume | 7 | |
journal issue | 2 | |
journal title | Journal of Computing and Information Science in Engineering | |
identifier doi | 10.1115/1.2738722 | |
journal fristpage | 167 | |
journal lastpage | 173 | |
identifier eissn | 1530-9827 | |
keywords | Design | |
keywords | Missiles | |
keywords | Ramjets | |
keywords | Shock (Mechanics) | |
keywords | Genetic algorithms AND Modeling | |
tree | Journal of Computing and Information Science in Engineering:;2007:;volume( 007 ):;issue: 002 | |
contenttype | Fulltext | |