Passive scalar (temperature) mixing with different orifice geometries is considered at low Reynolds number. The kinetic energy dissipation rate shows that the three jets achieve a self-similar state quickly compared to a nozzle jet. Scalar dissipation evolves faster to the self-preserving state than kinetic energy dissipation and the asymptotic value of the normalized kinetic and scalar dissipation on the jet centerline can be predicted. Taylor and Corrsin microscales start evolving linearly with x/D as early as x/D = 10. Normalized spectra using these length scales continue to evolve for the circular jet and collapse faster for the six-lobe jet, when Rλ reach a constant value. The scaling factor and range for the velocity and the scalar suggest that the scaling region “similar to the inertial range” reaches equilibrium before small scales reach complete equilibrium. The use of multilobe jets promotes the development toward a complete self-preserving state for the scalar field.
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November 2015
Research-Article
Effect of Orifice Geometry on the Development of Slightly Heated Turbulent Jets
Sehaba Madjid,
Sehaba Madjid
Faculty of Mechanical Engineering,
Oran 31000, Algeria
e-mail: majid_shb@hotmail.com
USTO-MB
,BP 1505 El M'Naouer
,Oran 31000, Algeria
e-mail: majid_shb@hotmail.com
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Sabeur Amina,
Sabeur Amina
Faculty of Mechanical Engineering,
Oran 31000,
e-mail: sabeuramina@hotmail.com
USTO-MB
,BP 1505 El M'Naouer
,Oran 31000,
Algeria
e-mail: sabeuramina@hotmail.com
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Azemi Benaissa
Azemi Benaissa
Department of Mechanical and
Royal Military College of Canada,
e-mail: benaissa-a@rmc.ca
Aerospace Engineering
,Royal Military College of Canada,
Kingston, ON K7K 7B4
, Canada
e-mail: benaissa-a@rmc.ca
Search for other works by this author on:
Sehaba Madjid
Faculty of Mechanical Engineering,
Oran 31000, Algeria
e-mail: majid_shb@hotmail.com
USTO-MB
,BP 1505 El M'Naouer
,Oran 31000, Algeria
e-mail: majid_shb@hotmail.com
Sabeur Amina
Faculty of Mechanical Engineering,
Oran 31000,
e-mail: sabeuramina@hotmail.com
USTO-MB
,BP 1505 El M'Naouer
,Oran 31000,
Algeria
e-mail: sabeuramina@hotmail.com
Azemi Benaissa
Department of Mechanical and
Royal Military College of Canada,
e-mail: benaissa-a@rmc.ca
Aerospace Engineering
,Royal Military College of Canada,
Kingston, ON K7K 7B4
, Canada
e-mail: benaissa-a@rmc.ca
Contributed by the Fluids Engineering Division of ASME for publication in the JOURNAL OF FLUIDS ENGINEERING. Manuscript received October 22, 2014; final manuscript received May 19, 2015; published online June 26, 2015. Assoc. Editor: Mark F. Tachie.
J. Fluids Eng. Nov 2015, 137(11): 111202 (8 pages)
Published Online: November 1, 2015
Article history
Received:
October 22, 2014
Revision Received:
May 19, 2015
Online:
June 26, 2015
Citation
Madjid, S., Amina, S., and Benaissa, A. (November 1, 2015). "Effect of Orifice Geometry on the Development of Slightly Heated Turbulent Jets." ASME. J. Fluids Eng. November 2015; 137(11): 111202. https://doi.org/10.1115/1.4030677
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