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Experimental Study of Jet Vectoring by using Counter Flow at Subsonic Speed in Circular Jet

by Ali Abdul Almuhsen Al-Asady, Ahmed Hikmat Faseeh
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International Journal of Computer Applications
Foundation of Computer Science (FCS), NY, USA
Volume 158 - Number 2
Year of Publication: 2017
Authors: Ali Abdul Almuhsen Al-Asady, Ahmed Hikmat Faseeh
10.5120/ijca2017912741

Ali Abdul Almuhsen Al-Asady, Ahmed Hikmat Faseeh . Experimental Study of Jet Vectoring by using Counter Flow at Subsonic Speed in Circular Jet. International Journal of Computer Applications. 158, 2 ( Jan 2017), 11-18. DOI=10.5120/ijca2017912741

@article{ 10.5120/ijca2017912741,
author = { Ali Abdul Almuhsen Al-Asady, Ahmed Hikmat Faseeh },
title = { Experimental Study of Jet Vectoring by using Counter Flow at Subsonic Speed in Circular Jet },
journal = { International Journal of Computer Applications },
issue_date = { Jan 2017 },
volume = { 158 },
number = { 2 },
month = { Jan },
year = { 2017 },
issn = { 0975-8887 },
pages = { 11-18 },
numpages = {9},
url = { https://ijcaonline.org/archives/volume158/number2/26879-2017912741/ },
doi = { 10.5120/ijca2017912741 },
publisher = {Foundation of Computer Science (FCS), NY, USA},
address = {New York, USA}
}
%0 Journal Article
%1 2024-02-07T00:03:44.865959+05:30
%A Ali Abdul Almuhsen Al-Asady
%A Ahmed Hikmat Faseeh
%T Experimental Study of Jet Vectoring by using Counter Flow at Subsonic Speed in Circular Jet
%J International Journal of Computer Applications
%@ 0975-8887
%V 158
%N 2
%P 11-18
%D 2017
%I Foundation of Computer Science (FCS), NY, USA
Abstract

An experimental investigation of fluidic jet vectoring using counter-flow method had been carried out in this current work. The experimental investigation included a set of experiments to examine the various effects of geometric variables on the thrust vectoring angle. These included Coanda surface radius R/d = (0.58823, 1.17647, 1.75471), secondary gap height h/d = (0.02941, 0.05882), and secondary mass flow ratio range of (0 ≤

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Index Terms

Computer Science
Information Sciences

Keywords

Thrust Vectoring Jet vectoring angle Coanda effect Counter-flow mass flow ratio

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