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Experimental and computational investigation into the use of co-flow fluidic thrust vectoring on a small gas turbine

Published online by Cambridge University Press:  03 February 2016

A. Banazadeh ,
F. Saghafi ,
M. Ghoreyshi  and
P. Pilidis
A. Banazadeh
Affiliation:
Department of Aerospace Engineering, Sharif University of Technology, Tehran, Iran
F. Saghafi
Affiliation:
Department of Aerospace Engineering, Sharif University of Technology, Tehran, Iran
M. Ghoreyshi
Affiliation:
Propulsion and Power, School of Engineering, Cranfield University, Bedford, UK
P. Pilidis
Affiliation:
Propulsion and Power, School of Engineering, Cranfield University, Bedford, UK
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Abstract

This paper presents the application of a relatively new technique of fluidic thrust-vectoring (FTV), named Co-flow, for a small gas-turbines. The performance is obtained via experiment and computational fluid dynamics (CFD). The effects of a few selected parameters including the engine throttle setting, the secondary air mass-flow rate and the secondary slot height upon thrust-vectoring performance are provided. Thrust vectoring performance is characterised by the ability of the system to deflect the engine thrust with respect to the delivered secondary air mass-flow rate. The experimental study was conducted under static conditions in an outdoor environment at Cranfield University workshop that was especially designed for this purpose. As part of this investigation, the system was modelled by CFD techniques, using Pointwise’s Gridgen software and the three-dimensional flow solver, Fluent. Also, Cranfield’s gas-turbine performance code (TurboMatch) was utilised to estimate boundary conditions for the CFD analysis with respect to the integrated nozzle. The presented technique is easy-to-use approach and offers better result for thrust-vectoring problems than previously published works. Experimental results do show the overall viability of the blowing slot mechanism as a means of vectoring the engine thrust, with the current configuration. Computational predictions are shown to be consistent with the experimental observations and make the CFD model a reliable tool for predicting Co-flow fluidic thrust-vectoring performance of similar systems.

Type
Research Article
Information
The Aeronautical Journal , Volume 112 , Issue 1127 , January 2008 , pp. 17 - 25
Copyright
Copyright © Royal Aeronautical Society 2008 

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