Numerical investigation of freestream flow effects on thrust vector control performance

Numerical investigation of freestream flow effects on thrust vector control performance

The current research attempted to apply a numerical investigation for external freestream-flow influence on thrust-vector control. The freestream-flow Mach numbers varying from 0.05 to 1.1 were studied at different flow conditions. Computational modeling and simulation of a converging diverging nozz...

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Bibliographic Details
Main Authors:	Farzad Forghany, Mohammad Taeibe-Rahni, Abdollah Asadollahi-Ghohieh
Format:	Article
Language:	English
Published:	Elsevier 2018-12-01
Series:	Ain Shams Engineering Journal
Online Access:	http://www.sciencedirect.com/science/article/pii/S2090447918300042

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