Home > Academics > Academic Units > Faculty of Engineering and Architecture (FoE&A) > Aerospace Engineering > Akshay Prakash
Ph.D.
Assistant Professor Grade-I
Aerospace Engineering
I am interested in developing and using existing CAE solvers to tackle industrial problems. I am also interested in modeling instabilities in fluid flows. My group has gained expertiese in CFD simulations using ANSYS FLuent, OpenFOAM (various solvers) and development of inhouse codes on Lattice Boltzmann Methods (for GPU parallel computations) and traditional ROE based compressible sovler (for CPU based parallel computations). I am open to explore problem with multi-physics interations.
Secondary subharmonic instability of hypersonic boundary layer in thermochemical equilibrium over a flat plate by Kumar C., Prakash A. Physics of Fluids 33 - (2021)
Nonlinear interaction among second mode resonance waves in high-speed boundary layers using the method of multiple scales by Kumar C., Prakash A. Physics of Fluids 34 014107- (2022)
High-Order Shock Fitting Methods for Simulation of Hypersonic Flow with Chemical and Thermal Nonequilibrium by Prakash A., Parsons N. , Wang X. , Zhong X. Journal of Computational Physics 230 - (2011)
Numerical Simulation of IPPE Target Geometry Flows by Prakash A., Kakarantzas S. , Bernardi D. , Micciche G. , Massaut V. , Knaepen B. Fusion Engineering and Design 88 - (2013)
Hydro-thermo analysis of Li flow over IFMIF geometry by Prakash A., Kakarantzas S. , Bernardi D. , Micciche G. , Knaepen B. Fusion Engineering and Design 89 - (2014)
A comparative study of three-dimensional discrete velocity set in LBM for turbulent flow over bluff body by Agarwal A., Prakash A. Journal of the Brazilian Society of Mechanical Sciences and Engineering 43 - (2021)
Numerical investigation of flow behavior in double-rushton turbine stirred tank bioreactor by Agarwal A., Singh G. , Prakash A. Materialstoday: Proceedings 43 51-57 (2021)
A comparative study of bounce-back and immersed boundary method in LBM for turbulent flow simulation by Agarwal A., Prakash A. Materials Today 28 - (2020)
Numerical Investigation of the Effect of Fuel Injection Scheme on the Performance of SCRAM Jet Combustor KCSTC
Numerical Investigation of the Effect of Fuel Injection Scheme on the Performance of SCRAM Jet Combustor ISRO, INDIA
Aero-Thermo-Elastic Analysis of Hypersonic Vehicle Aeronautics R and D Board
Shambhu Kumar Tati
Area of Research: Fluid Mechanics
