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Jet mixing into a heated cross flow in a cylindrical duct - Influence of geometry and flow variations
Author(s) -
M. S. Hatch,
W. A. Sowa,
G. Samuelson,
J. D. Holdeman
Publication year - 1992
Publication title -
38th aerospace sciences meeting and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.1992-773
Subject(s) - body orifice , mechanics , geometry , duct (anatomy) , physics , mixing (physics) , penetration (warfare) , momentum (technical analysis) , jet (fluid) , injector , flux (metallurgy) , materials science , optics , thermodynamics , mechanical engineering , mathematics , engineering , medicine , pathology , quantum mechanics , finance , operations research , metallurgy , economics
To examine the mixing characteristics of jets in an axi-symmetric can geometry, temperature measurements were obtained downstream of a row of cold jets injected into a heated cross stream. Parametric, non-reacting experiments were conducted to determine the influence of geometry and flow variations on mixing patterns in a cylindrical configuration. Results show that jet to mainstream momentum flux ratio and orifice geometry significantly impact the mixing characteristics of jets in a can geometry. For a fixed number of orifices, the coupling between momentum flux ratio and injector determines (1) the degree of jet penetration at the injection plane, and (2) the extent of circumferential mixing downstream of the injection plane. The results also show that, at a fixed momentum flux ratio, jet penetration decreases with (1) an increase in slanted slot aspect ratio, and (2) an increase in the angle of the slots with respect to the mainstream direction.

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