1 / 9

NLTE simulations with CRASH code and related issues Fall 2011 Review

NLTE simulations with CRASH code and related issues Fall 2011 Review. Igor Sokolov [with Michel Busquet and Marcel Klapisch (ARTEP)]. Reaction rates in xenon are a possible issue for CRASH . LTE happens when

enoch
Download Presentation

NLTE simulations with CRASH code and related issues Fall 2011 Review

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. NLTE simulations with CRASH code and related issuesFall 2011 Review Igor Sokolov [with Michel Busquet and Marcel Klapisch (ARTEP)]

  2. Reaction rates in xenon are a possible issue for CRASH • LTE happens when • radiative recombination (red curve) << 3-body collisional recombination (green curve) • Then collisions ensure that Z=Z(Te) only. • Non-LTE happens when • radiation recombination dominates over 3-body recombination • The coronal model then applies: one-source-two-sinks of free electrons, which affect the ionization degree. • For optically thin media, of course • Prof. G.A.Moses raised this issue CRASH density 50 eV Xe Radiative recombination LTE Reaction rate Dielectronic 3-body 1020 1022 1012 Atomic density [per cm3] 1014 1016 1018

  3. NonLTEmay impact the CRASH problem •energy balance : for same Etot, more in electron kinetic energy, and less in ionization "internal" energy • thermal conduction : as average charge is lower, electron conduction (and laser absorption) is reduced • radiative energy : • less coupling of radiation with matter • X-ray conversion of Elaser reduced • x-ray precursor (of shock wave, ...) has larger extent

  4. Principle of the RADIOM model • • Non-LTE of charge state distribution (and excited states to some extent) • is mimicked by an "ionization temperature" Tz • We are able to derive numerically Tz from Ne, Te, {hnu,Erad/Brad} • Non-LTE total energy is a function of Eint(Tz), Zbar(Tz), Te (and ro) :

  5. RADIOM reduces the effective ionization in a manner consistent with the SCROLL model

  6. RADIOM algorithmwith direct EOS done CRASH in progress ro Te {Erad/Brad} estimated Ne Eeff Z* CALTZ EOS(Tz) Tz Zdif= |Z*Ni-Ne| ≈ 0 > 0 ro, Ne [Te],Tz {Erad/Brad} Etot Ptot Cv correct EOS handling Abs. AND Emiss. opacities LUT(ro,Tz) correct Opacities Abs.Coef. Emis.Coef.

  7. The coronal model is not enough for CRASH • In the (solar) corona the “back-lighter” (the photosphere) has a radiation temperature much LOWER than Te in the corona (half eV vs hundreds eV). Contrary to our case. • We may need more electrons, while the coronal model gives us less electrons. • Need to implement the RADIOM/CRASH coupling for the out-of-equilibrium HOT radiation (hundreds eV vs tens eV). • This isnow in progress.

  8. We have made progress on Non-LTE • RADIOM and CRASH codes are coupled now. • “Coronal model” fully implemented • More complete model is under testing • Implementing these models allows us to quantify another source of uncertainties in the CRASH predictions

More Related