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Nitin Dhamankar
Nitin Dhamankar
HPC Performance Architect, Intel Corporation
Verified email at intel.com
Title
Cited by
Cited by
Year
Overview of Turbulent Inflow Boundary Conditions for Large-Eddy Simulations
NS Dhamankar, GA Blaisdell, AS Lyrintzis
AIAA Journal, 2017
1862017
Digital filter-based turbulent inflow generation for jet aeroacoustics on non-uniform structured grids
NS Dhamankar, CS Martha, Y Situ, KM Aikens, GA Blaisdell, AS Lyrintzis, ...
AIAA Paper, 2014
302014
Equilibrium wall model for large eddy simulations of jets for aeroacoustics
KM Aikens, NS Dhamankar, CS Martha, Y Situ, GA Blaisdell, AS Lyrintzis, ...
AIAA paper 180, 2014
192014
Boundary conditions towards realistic simulation of jet engine noise
NS Dhamankar
M.S.E. Thesis, Purdue University, 2012
142012
Implementation of a Wall-Modeled Sharp Immersed Boundary Method in a High-Order Large Eddy Simulation Tool for Jet Aeroacoustics
NS Dhamankar, GA Blaisdell, AS Lyrintzis
54th AIAA Aerospace Sciences Meeting, 0257, 2016
122016
Implementation of a Sharp Immersed Boundary Method in a 3-D Multi-block Large Eddy Simulation Tool for Jet Aeroacoustics
NS Dhamankar, GA Blaisdell, AS Lyrintzis
AIAA Paper, 2015
122015
Analysis of Turbulent Jet Flow and Associated Noise with Round and Chevron Nozzles using Large Eddy Simulation
NS Dhamankar, GA Blaisdell, AS Lyrintzis
22nd AIAA/CEAS Aeroacoustics Conference, Lyon, France, 2016
112016
A simple extension of digital filter-based turbulent inflow to non-uniform structured grids
NS Dhamankar, GA Blaisdell, AS Lyrintzis
Aerospace Science and Technology 56, 29-33, 2016
62016
An Immersed Boundary Method for Efficient Computational Studies of Nozzles Designed to Reduce Jet Noise
N Dhamankar
Ph.D. Thesis, Purdue University, 2016
52016
The Use of Petaflop Computing for Jet Noise Predictions
CS MARTHA, Y SITU, N DHAMANKAR, AS LYRINTZIS, GA BLAISDELL, ...
2012
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