Carte Triangular Tabs for Supersonic Jet Control Arun Kumar P.

Triangular Tabs for Supersonic Jet Control

An Experimental Study

Autor: Arun Kumar P.
Limbă: engleză
Legare: Carte broșată
Editura: Scholars' Press
Disponibilitate: În depozitul extern
Expediem în 5-8 zile
430.58 lei
An experimental investigation has been carried out to study the mixing promoting efficiency of right...

Informații despre carte

Limbă
engleză
Legare
Carte - Carte broșată
Publicat
2013
Pagini
216
EAN
9783639702316
ISBN
363970231X
Enbook ID
07043873
Editura
Greutate
322
Dimensiuni
152 x 229 x 12

Descriere completă

An experimental investigation has been carried out to study the mixing promoting efficiency of right-angled and isosceles triangular tabs with sharp and truncated vertices. The mixing promotion caused by two identical triangular tabs, offering a geometrical blockage of 2.5% each, placed at the exit of a Mach 2 circular nozzle, was studied in the presence of adverse and marginally favourable pressure gradients. The results of the present study demonstrate the validity of the hypothesis that, the triangular tabs shedding vortices of continuously varying sizes is a better mixing promoter than the rectangular tabs, shedding vortices of uniform size. Furthermore, the truncated vertex triangular tab is found to be a better mixing promoter than the sharp vertex triangular tab, at all levels of expansion of the present study.

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