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Handout 1 - Clemson University

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p e+- dV +Jp e+ ii -nidS =- pii -idS<br />

dt V 2 ) s( 2)<br />

Equation 3.2-3<br />

where a volume V with surface S is assumed to be fixed in space, and ,i is the normal<br />

vector on a portion dS of the surface S<br />

The above governing equations that no body assume forces are acting on the fluid<br />

particles and no heat transfer or radiation is taking place. These assumptions are valid<br />

since none of these effects are known to play a crucial role in blast wave propagation<br />

[32].<br />

We will consider a normal shock as the one shown in Figure 3.2-1. The shock is<br />

propagating (left illustration) with a velocity of Us into a uniform stream with fluid<br />

particle velocity ul, while the particle velocity behind it is u2. A more convenient way to<br />

handle this phenomenon is to consider the right image of Figure 3.2-1, where a<br />

reference moving frame with Us velocity is considered. Consequently, the velocities in<br />

front and behind the shock front are now U1=u1+Us and U2=u2+Us respectively.<br />

u10<br />

Us<br />

(A)<br />

Moving Shock<br />

U2<br />

Figure 3.2-1: Moving and stationary shock wave [26]<br />

U 1=u 1 + Us U 2=u 2 + Us<br />

(B)<br />

Stationary Shock

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