Changes between Version 47 and Version 48 of 1DPulsedJets

Timestamp:

03/30/12 12:51:26 (13 years ago)

Author:

ehansen

Comment:

—

1DPulsedJets

@@ -222 +222 @@
 
 === Equations ===
-The shock jump equations for a stationary shock are used to solve for the initial post-shock values.  The post-shock velocity v2 can be written as:
-
-
-where v1 is the ambient velocity, and M is the ambient mach number.  Remember that the mach number M = v1/c where c is the ambient sound speed, and [[latex($c = \sqrt{\frac{\gamma P1}{\rho1}}$)]] where P1 is ambient pressure, and [[latex($\rho1$)]] is ambient density.
-
-The post-shock density and pressure ([[latex($\rho2$)]] and P_2_ respectively) can be found by using mass flux and momentum flux conservation across the shock:
+The shock jump equations for a stationary shock are used to solve for the initial post-shock values.  The post-shock velocity v,,2,, can be written as:
+
+
+where v,,1,, is the ambient velocity, and M is the ambient mach number.  Remember that the mach number M = v,,1,,/c where c is the ambient sound speed, and [[latex($c = \sqrt{\frac{\gamma P_{1}}{\rho_{1}}}$)]] where P,,1,, is ambient pressure, and [[latex($\rho_{1}$)]] is ambient density.
+
+The post-shock density and pressure ([[latex($\rho_{2}$)]] and P,,2,, respectively) can be found by using mass flux and momentum flux conservation across the shock:
 
 These post-shock values become the boundary conditions for the fluid equations in the cooling region:
@@ -235 +235 @@
 [[BR]]
 === Initial Parameters ===
-n1 = 60 particles/cc
-
-v1 = 10^7^ cm/s
-
-T1 = 10^4^ K
+n,,1,, = 60 particles/cc
+
+v,,1,, = 10^7^ cm/s
+
+T,,1,, = 10^4^ K
 
 For analytic cooling,