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Measurements of turbulent inclined plane dual jets
Authors:C. S. Wang  Y. F. Lin  M. J. Sheu
Affiliation:(1) Civil Engineering Department, Chung Yuan Christian University, Chung Li Taiwan, 32023, Republic of China;(2) Present address: International Superior Associates Corp., 45373 White Pines Drive, 48375 Novi, MI, USA
Abstract:
Measurements of mean velocities, flow direction, velocity fluctuations and Reynolds shear stress were made with a split film probe of hot wire anemometer to investigate the interactions created by two air jets issuing from two identical plane inclined nozzles. The reverse flow was detected by using the split film probe and observed by flow visualization. Experimental results with an inclined angle of 9° are presented in the paper. Some experimental results with an inclined angle of 27° are presented to investigate the effect of inclination on the flow field.Mean velocities approach self-preservation in both the converging region and the combining region. Velocity fluctuations and Reynolds shear stress approach self-preservation in the combining region only. The spreads of jet and the square of the decay of maximum mean velocity increase linearly as the distance from the nozzle exit increases.List of symbols D nozzle width - h nozzle height - J momentum of jet - J0 momentum of jet at nozzle exit - M mass flow rate - M0 mass flow rate at nozzle exit - S nozzle spacing - U, V mean velocities in the X and Y axis respectively - Um maximum axial velocity - U0 axial velocity at nozzle exit - u, v velocity fluctuations in the X and Y axis respectively - uprime, vprime r.m.s. of u and v - 
$$overline {uupsilon } $$
Reynolds shear stress - X, Y Cartesian coordinates - Xm, Ym coordinates at the location of maximum axial velocity - y0.5 distance from the location of maximum axial velocity to the location where the velocity is half of maximum axial velocity - theta inclined angle - eegr yY/S - phiv Reynolds stress correlation coefficient 
$${text{(}}overline {uupsilon } /u'upsilon '{text{)}}$$
- C.P combining point - max maximum value - M.P merging point - o nozzle exit plane - V.C vortex center
Keywords:
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