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Find the upstream Mach number if there is a entropy increase across the normal shock wave of $220\,J/\left( {kg.K} \right)$ .
Find the upstream Mach number if there is an entropy increase across the normal shock wave of $220\,J/\left( {kg.K} \right)$ .
Mach number

normal shock waves

Shock waves

thermodynamics

techAir Asked on 11th March 2021 in Aerodynamics.
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A flow passes through a normal shock wave has a pressure, temperature and Mach number of $1\,atm,\,295\,K$ and $2.8$ upstream of the shock wave. Find ${P_2},{T_2},\,{\rho _2},\,{M_2},{P_{02}}$ and ${T_{02}}$ downstream of the shock wave.
A flow passes through a normal shock wave has a pressure, temperature and Mach number of $1\,atm,\,295\,K$ and $2.8$ upstream …
airspeed

normal shock waves

Shock waves

Supersonic flow

Kumar59 Asked on 11th March 2021 in Aerodynamics.
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