Annexv

Page 1

Annex V

AV- Theory of Vented Deflagration, Grigorash 2002 How to obtain the derivation equations of vented deflagration used in this model is explained below. This theory was developed by Grigorash in 2002. First of all, let us refer the real distorted flame front area Ff(t) at any moment t of time to the surface Fs(t), see Eq. (AV-1), where rb is the radius of the sphere occupied by burnt gas. The ratio of both flame front areas is called turbulence factor (see Eq. (AV-2)). Fs (t) = 4 πo rb2 F (t) χ(t) = f Fs (t)

(AV-1) (AV-2)

The dependence of burning velocity is on the temperature and pressure of the gaseous mixture, Eq. (AV-3). m

T  p Su = Sui  u     Tui   pi 

n

(AV-3)

From the adiabatic equation pVγ = cte together with the ideal gas state equation, one can easily derive the following relationship, Eq. (AV-4).

T p =  Ti  pi 

γ−1

γ

1− 1 γ

(AV-4)

This proportion allows one to express the burning velocity in the form Su = Sui πε

(AV-5)

Where the values of thermokinetic factor ε = m + n – m/γu along with the burning velocity can be found in literature. Defining σu as Eq. (AV-6), where ρi and ρu are the initial and the current unburnt gas densities and taking the adiabatic equation written now in the form p(m/ρ)γ = cte, for both the initial and the current densities, one can see that σu = π1/ γ u

(AV-6)

For defining σb, we denote nu = mu/mi and nb = mb/mi the relative masses; wu = Vu/V and wb = Vu/V the relative volumes of unburnt and burnt gases. Volume conservation within the gas gives wu + wb = 1. Therefore, for the average relative density of burnt gases throughout the enclosure we can obtain Eq. (AV7).

A-49


Turn static files into dynamic content formats.

Create a flipbook
Issuu converts static files into: digital portfolios, online yearbooks, online catalogs, digital photo albums and more. Sign up and create your flipbook.