SIMULATION OF 3-D TURBULENT JET-INTO-CROSS FLOW, USING HYBRID LES/URANS APPROACH

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GHODSI S.R.; TAEIBI RAHNI M.; RAMEZANI ZADEH M.; JARRAH BASHI D.

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Paper Information

Journal: Journal of Aerospace Mechanics Year:2011 | Volume:7 | Issue:3 (25) Page(s): 39-52

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Title

SIMULATION OF 3-D TURBULENT JET-INTO-CROSS FLOW, USING HYBRID LES/URANS APPROACH

Author(s)

GHODSI S.R. | TAEIBI RAHNI M. | RAMEZANI ZADEH M. | JARRAH BASHI D. | Issue Writer Certificate

Keywords

HYBRID LES/URANSQ2

JET-INTO-CROSS FLOWQ2

VELOCITY RATIOQ2

Abstract

In this paper the results of simulation of a 3-D turbulent normal JET-INTO-CROSS FLOW at Reynolds number of 4700, based on the diameter and velocity of the jet, using HYBRID LES/URANS approach, are presented. The computational methodology is based on finite volume and the grid is non-uniform and staggered. The results show that the HYBRID LES/URANS approach can well predict complex flows. Furthermore, the flows upstream and downstream of the jet were affected by variation of the VELOCITY RATIO.

Cites

STUDY OF DIFFERENT TYPES OF HYBRID LES/RANS APPROACH

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APA: Copy

GHODSI, S.R., TAEIBI RAHNI, M., RAMEZANI ZADEH, M., & JARRAH BASHI, D.. (2011). SIMULATION OF 3-D TURBULENT JET-INTO-CROSS FLOW, USING HYBRID LES/URANS APPROACH. AEROSPACE MECHANICS JOURNAL, 7(3 (25)), 39-52. SID. https://sid.ir/paper/101901/en

Vancouver: Copy

GHODSI S.R., TAEIBI RAHNI M., RAMEZANI ZADEH M., JARRAH BASHI D.. SIMULATION OF 3-D TURBULENT JET-INTO-CROSS FLOW, USING HYBRID LES/URANS APPROACH. AEROSPACE MECHANICS JOURNAL[Internet]. 2011;7(3 (25)):39-52. Available from: https://sid.ir/paper/101901/en

IEEE: Copy

S.R. GHODSI, M. TAEIBI RAHNI, M. RAMEZANI ZADEH, and D. JARRAH BASHI, “SIMULATION OF 3-D TURBULENT JET-INTO-CROSS FLOW, USING HYBRID LES/URANS APPROACH,” AEROSPACE MECHANICS JOURNAL, vol. 7, no. 3 (25), pp. 39–52, 2011, [Online]. Available: https://sid.ir/paper/101901/en

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