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Computational Fluid Dynamics

 

Viscous Attenuation of a Detonation Wave Propagating in a Channel

P. Ravindran, R. Bellini, T.-H. Yi, Ph.D. and F.K. Lu, Ph.D.

Motivation for Research

Euler vs. Navier-Stokes
  • Detonation wave propogation in a tube similar to Sod shock tube problem
  • Boundary layer growth due to viscosity has long been neglected due to complexity of the simulation
  • Shock-Boundary layer interaction remains poorly understood
  • Faster computing power - preference of Navier Stokes equations over the Euler equations
  • Transport processes such as viscosity can be included in the governing equations
 
Governing Equations Numerical Model
  • Governing equations are modeled by coupling thermodynamic processes, chemical reactions, and fluid dynamics
  • Flow is assumed to be thermally perfect with non-equilibrium finite-rate chemistry
  • Elementary reaction mechanism obtained from GRI-MECH database
  • Viscosity, diffusion, and thermal conductivity obtained from classical kinetic theory
  • Discretization using Finite Volume formulation retaining integral form
  • Convective fluxes approximated by
    flow quantities left and right of a cell
  • Viscous fluxes computed by averaged variables at a face
  • Roe second order scheme for multi-species, thermally perfect gas
  • Higher order approximations using
    MUSCL approach
  • Two-step Runge-Kutta scheme with
    second order accuracy for temporal
    discretization
  • Transport terms are evaluated by Green’s theorem
  • Evaluation of temperature at cell when species density is updated for thermally perfect gas
Results and Conclusions  
  • 50 cm long and 10 cm high channel
    Domain discretized into 100X150 cells
  • Grids are clustered near the walls to
    capture BL
  • Adiabatic wall conditions with inflow
    supersonic
  • Pressure at outlet set at 1 atm
  • Premixed H2-Air at 2 atm and 500 K
    with incoming Mach 2.0
  • Mixture ignited by localized hot-spot at 30 atm and 3000 K located 0.1 m into channel at left end
  • Results show wave propagation delayed for viscous case

 

Parallel Algorithm for Detonation Wave Simulation

P. Ravindran and F. K. Lu, Ph.D.
Need for Parallel Computing Why MPI?
  • Increasing reliance on CFD to produce
    time accurate simulations of physical
    phenomenon
  • Accurate simulations of complex phenomena such as detonations need immense computational requirements due to time constraints
  • Expensive to build supercomputers, cost effective for parallel computers
  • MPI (Message Passing Interface) is used due to it language-independence, scalable nature and portability
  • Provides virtual topology, synchronization and communication between processors
  • Ability to initiate point-to-point communication without network overload
Simulation LONESTAR - DELL Cluster
  • Inviscid Euler model assuming thermally
    perfect gas
  • Two temperature model
  • H2 – Air model with conditions 2 atm,
    500K and incoming Mach number 2.0
  • Localized hotspot of 30 atm and 3000 K Grid domain – 100X150 cells
  • MPI 2.0 implementation with collective
    communication
  • Scaleup indicates good scalability with
    memory usage increasing linearly with
    increasing processors
  • Bandwidth blockage noticed beyond 96
    processors: higher the processors, more time spent in communication
  • Part of NSF TeraGrid
  • Peak FLOPS – 55.5 TFLOPS
  • Total no: of nodes – 1300
  • Node – Dell Blade 1955, 4 cores/node
  • Network - InfiniBand