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Impact of fuel supply impedance and fuel staging on gas turbine ...

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3.2 Linear acoustic equati<strong>on</strong>s<br />

p ′<br />

ρ 0 c<br />

= f (ξ)+ g (η)= f (x− c t )+ g (x+ c t ). (3.21)<br />

The soluti<strong>on</strong> p ′ <str<strong>on</strong>g>of</str<strong>on</strong>g> the latter equati<strong>on</strong> is, in general, normalized by the characteristic<br />

<str<strong>on</strong>g>impedance</str<strong>on</strong>g> ρ 0 c. f <str<strong>on</strong>g>and</str<strong>on</strong>g> g are the so-called Riemann Invariants <str<strong>on</strong>g>and</str<strong>on</strong>g> are<br />

determined by boundary or initial c<strong>on</strong>diti<strong>on</strong>s. The Riemann Invariants represent<br />

physically waves, which are traveling with speed <str<strong>on</strong>g>of</str<strong>on</strong>g> sound c in the right or<br />

positive x-directi<strong>on</strong> (f ) or rather in the left or negative directi<strong>on</strong> (g ) as shown<br />

in Fig. 3.1.<br />

g<br />

f<br />

x<br />

Figure 3.1: Riemann Invariants f <str<strong>on</strong>g>and</str<strong>on</strong>g> g traveling in positive <str<strong>on</strong>g>and</str<strong>on</strong>g> negative x-<br />

directi<strong>on</strong><br />

The acoustic velocity u ′ can be obtained from the acoustic pressure p ′<br />

(Eqn. (3.21)) <str<strong>on</strong>g>and</str<strong>on</strong>g> the linearized momentum equati<strong>on</strong> (3.17):<br />

u ′ = f (x− c t )− g (x+ c t ). (3.22)<br />

Using Eqn. (3.21) <str<strong>on</strong>g>and</str<strong>on</strong>g> (3.22), the Riemann Invariants can be c<strong>on</strong>versely expressed<br />

in terms <str<strong>on</strong>g>of</str<strong>on</strong>g> p ′ <str<strong>on</strong>g>and</str<strong>on</strong>g> u ′ :<br />

f = 1 ( p<br />

′<br />

)<br />

2 ρ 0 c + u′ , (3.23)<br />

g = 1 ( p<br />

′<br />

)<br />

2 ρ 0 c − u′ . (3.24)<br />

49

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