*HEADING
 1D transient wave propagation in an acoustic medium with CLOAD on dof 8. 
 ACAX3
 Verification problem: Transient Dynamics Tests
**
** C = root (K/rho)= 343.05 m/s   K=bulk mod, rho=density.  
**
** Analytic solution to prescribed constant acceleration of a0 at x=0
** 
** p(z,t) = (K a0 / c^2) (ct - z)  for z < ct
**        = 0  			   for z > ct
** 
*PREPRINT,ECHO=NO,HISTORY=NO,MODEL=YES
*NODE, Nset=ODB_NSET
    1, 0,
  101, 0, 1.,
  501, .5e-2,0.
  601, .5e-2,1.
 1001, 1.e-2,0.
 1101, 1.e-2,1.
*NGEN,NSET=CHANNEL
    1,101
 1001,1101
*NSET,NSET=SAMPLE,GENERATE
 1,101
*NSET,NSET=LOAD
 1,1001
*ELEMENT,TYPE=ACAX3
 1,1,1002,2
 2,1,1001,1002
*ELGEN,ELSET=CHANNEL
 1,100,1,2
 2,100,1,2
*SOLID SECTION,MATERIAL=AIR,ELSET=CHANNEL
 1.e-2, 
** Cross-section is 1.0e-4 * Pi
**
*MATERIAL,NAME=AIR
*DENSITY
 1.21,
*ACOUSTIC MEDIUM,BULK MODULUS
 0.1424E6,
**
*RESTART,WRITE
**
**
** Sets added by addodb
**
*Elset,Elset=ODB_ESET
CHANNEL,
**
**
*Nset, Nset=ODB_NSET
ODB_NSET, CHANNEL, SAMPLE, LOAD
**
**
*STEP,INC=1000
*DYNAMIC
.0001,.0044
** Define nonreflective boundary at z=1
*IMPEDANCE
 199,I2
**
**
** Prescribe volume acceleration inwards
**     of  a0=1.
**     Distribute to each node on edge according to:.
**  [1/3, 2/3] *area
*CLOAD
 1,8,1.04719755e-4
 1001,8,2.09439510e-4
**
*EL PRINT,FREQ=0
*NODE PRINT,NSET=SAMPLE,FREQ=22
 POR,
*NODE FILE,NSET=SAMPLE,FREQ=22
 POR,
*OUTPUT,FIELD,VARIABLE=PRESELECT,OP=ADD,FREQUENCY=9999
*OUTPUT,FIELD, OP=ADD,Frequency=22
*NODE OUTPUT,NSET=SAMPLE
 POR,
*OUTPUT,HISTORY,OP=ADD,Frequency=22
*NODE OUTPUT,NSET=SAMPLE
 POR,
*ENDSTEP