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Numerical simulation of detonation failure and re-initiation in bifurcated tubes Numerical simulation of detonation failure and re-initiation in bifurcated tubes

Numerical simulation of detonation failure and re-initiation in bifurcated tubes - PowerPoint Presentation

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Numerical simulation of detonation failure and re-initiation in bifurcated tubes - PPT Presentation

Centre for Fire and Explosion Studies School of Mechanical and Automotive Engineering Kingston University London Centre for Fire and Explosion Studies A Heidari and JX Wen Detonation ID: 721470

bifurcated detonation simulation numerical detonation bifurcated numerical simulation propagation atm shock modelling diffusion equations due tube monotone grid failure

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Slide1

Numerical simulation of detonation failure and re-initiation in bifurcated tubes

Centre for Fire and Explosion StudiesSchool of Mechanical and Automotive Engineering, Kingston University London

Centre for Fire and Explosion Studies

A.

Heidari

and J.X.

WenSlide2

Detonation

propagation in bifurcated tubesSlide3

Outline

IntroductionDeflagration, Detonation and DDT

Equations, Reaction and Modelling approach

Code development and testing

Detonation

simulation

Summery Slide4

Combustion waves

Detonations

DDT

Laminar

flames

Turbulent

flames

3 m/s

800 m/s

2000 m/s

low speed

High speed

Deflagrations

Detonations

U

0.1

atm

5

atm

20

atm

P

Diffusion of mass and energy

Auto-ignition due to shock heatingSlide5

Multidimensional, time-dependent, compressible reactive

Navier–Stokes equations Modelled:

chemical reactions

molecular diffusion

thermal conduction

viscosity

Governing equations & Numerical modelling

 Slide6

Turbulence & Numerical modelling

Discretization: Gaussian finite volume integration

Time derivatives: Crank-Nicholson

Van Leer (TVD) scheme for shock capturing

Monotone Integrated Large Eddy

Simulation (MILES)

“monotone

schemes have an inherent truncation error that acts as a numerical diffusion, which can emulate the effects of physical

viscosity”Slide7

Grid independency testSlide8

Testing the solver for Detonation and Deflagration wavesSlide9

Structure of detonation frontSlide10

Boundary and initial conditions

Smallest grid size: 10 micron, structured (AMR)20 grid points across the detonation half reaction length Boundary conditions: no-slip reflecting boundaries

Fuel:

Hydrogen-Oxygen-diluent

mixture

Ignition: a region of high temperature and pressure (T= 2500 K, p= 15

atm

)

Single step reactions, 16

kPa

, 300 K initialSlide11

Detonation propagation in a bifurcated tubeSlide12

Detonation propagation in a bifurcated tube

C. J. WANG, S. L. XU AND C. M. GUO, “

Study on gaseous detonation propagation in a bifurcated tube

”, Journal of Fluid Mechanics (2008), 599: 81-110Slide13

Detonation failure due to shock diffraction Slide14

Detonation re-initiationSlide15

Detonation propagation in a bifurcated sectionSlide16

Summery

A solver for simulation deflagration, flame acceleration and detonation is developed and validated. Monotone Integrated Large Eddy Simulation (MILES

) is used

Structured mesh and Adaptive Mesh Refinement is used to increase the efficiency and reduce the computational cost.

Good agreement with experiments and other numerical works is achieved.

Detonation failure due to wave diffraction and subsequent detonation re-initiation is simulated and compared against the experimental observation of Wang et. al.Slide17

Thank you