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Direct Numerical Simulation of a Coolant Jet in a Periodic CrossflowA Direct Numerical Simulation of a coolant jet injected normally into a periodic crossflow is presented. The physical situation simulated represents a periodic module in a coolant hole array with a heated crossflow. A collocated finite difference scheme is used which is fifth-order accurate spatially and second-order accurate temporally. The scheme is based on a fractional step approach and requires the solution of a pressure-Poisson equation. The simulations are obtained for a blowing ratio of 0.25 and a channel Reynolds number of 5600. The simulations reveal the dynamics of several large scale structures including the Counter-rotating Vortex Pair (CVP), the horse-shoe vortex, the shear layer vortex, the wall vortex and the wake vortex. The origins and the interactions of these vortical structures are identified and explored. Also presented are the turbulence statistics and how they relate to the flow structures.
Document ID
19990008658
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sharma, Chirdeep
(Louisiana State Univ. Baton Rouge, LA United States)
Acharya, Sumanta
(Louisiana State Univ. Baton Rouge, LA United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1998
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
GRC-E-DAA-TN10127
E-11402
NASA/CR-1998-208674
Report Number: GRC-E-DAA-TN10127
Report Number: E-11402
Report Number: NASA/CR-1998-208674
Meeting Information
Meeting: International Mechanical Engineering Congress and Exposition
Location: Anaheim, CA
Country: United States
Start Date: November 15, 1998
End Date: November 20, 1998
Funding Number(s)
PROJECT: RTOP 538-12-10
CONTRACT_GRANT: NAG3-1641
Distribution Limits
Public
Copyright
Public Use Permitted.
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