Numerical Simulation of a Flowfield Around a Hypersonic Missile with Lateral Jets
<p> This work uses computational fluid dynamics to study the flowfield around a hypersonic missile with two lateral jets to provide control in place of control surfaces. The jets exhaust an H<sub>2</sub>-O<sub>2</sub> mixture at Mach number of 2.9 with a jet pressure ra...
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| Language: | EN |
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Florida Atlantic University
2017
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| Online Access: | http://pqdtopen.proquest.com/#viewpdf?dispub=10605920 |