Research Article

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

by  Ali Abdul Almuhsen Al-Asady, Ahmed Hikmat Faseeh
journal cover
International Journal of Computer Applications
Foundation of Computer Science (FCS), NY, USA
Volume 158 - Issue 2
Published: Jan 2017
Authors: Ali Abdul Almuhsen Al-Asady, Ahmed Hikmat Faseeh
10.5120/ijca2017912741
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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 },
                        year    = { 2017 },
                        volume  = { 158 },
                        number  = { 2 },
                        pages   = { 11-18 },
                        doi     = { 10.5120/ijca2017912741 },
                        publisher = { Foundation of Computer Science (FCS), NY, USA }
                        }
                        %0 Journal Article
                        %D 2017
                        %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%T 
                        %J International Journal of Computer Applications
                        %V 158
                        %N 2
                        %P 11-18
                        %R 10.5120/ijca2017912741
                        %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
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Keywords

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

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