Experimental and numerical research of a supersonic planar thrust vectoring nozzle via mechanical tabs

Experimental and numerical research of a supersonic planar thrust vectoring nozzle via mechanical tabs

Wind tunnel cold flow tests were conducted, using the convergentdivergent two-dimensional nozzle, with a tab as the obstacle at the nozzle exit area. This geometry is applied in thrust vector control systems for missiles. During the variation of some of the most influential geometry parameters in th...

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Bibliographic Details
Main Authors: Živković Saša, Milinović Momčilo, Adamec Norbert
Format: Article
Language:English
Published: University of Belgrade - Faculty of Mechanical Engineering, Belgrade 2014-01-01
Series:FME Transactions
Subjects:
tvc
two-dimensional
nozzle
wind tunnel
separated flow
cfd
turbulence model
Online Access:https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2014/1451-20921403205Z.pdf

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