The default integration time for the EPM ( timeFinal in Integrate.cpp line 209) is set to 2000 seconds. This timeframe of ~33 minutes is much longer than the generally accepted timeframe for contrail jet and vortex sinking (~3 min). [1]
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double timeFinal = 2.0E+03; |
Additionally, the differential equations being solved generally reach a quasi-steady state by around 300s.
I would suggest this parameter be added as a user input for improved transparency to the user. For diagnostic reasons I would also suggest the epm-output.nc file include the time resolved arrays for the reported parameters instead of just scalar values at t=2000s.
[1] Contrail cirrus, in Cirrus, edited by D. K. Lynch, K. Sassen, D. O. Starr and G. L. Stephens, pp. 233, Oxford Univ.
The default integration time for the EPM (
timeFinalinIntegrate.cppline 209) is set to 2000 seconds. This timeframe of ~33 minutes is much longer than the generally accepted timeframe for contrail jet and vortex sinking (~3 min). [1]APCEMM/Code.v05-00/src/EPM/Models/Original/Integrate.cpp
Line 209 in 7a2ec32
Additionally, the differential equations being solved generally reach a quasi-steady state by around 300s.
I would suggest this parameter be added as a user input for improved transparency to the user. For diagnostic reasons I would also suggest the
epm-output.ncfile include the time resolved arrays for the reported parameters instead of just scalar values at t=2000s.[1] Contrail cirrus, in Cirrus, edited by D. K. Lynch, K. Sassen, D. O. Starr and G. L. Stephens, pp. 233, Oxford Univ.