SLIDE 1 CLEAR
Evolution of a radiative shock system in a high- energy-density regime
Carolyn C. Kuranz
University of Michigan Center for Radiative Shock Hydrodynamics Center for Laser Experimental Astrophysical Research TST 2013
SLIDE 2 CLEAR
Shock waves become radiative when…
- Radiative energy flux would exceed incoming material energy flux
Where post-shock temperature is proportional to us
2
The ratio of these energy fluxes is proportional to us
5/ρo
Implying threshold velocities ….
Material
Density
Threshold velocity 60 µm/ns (km/s) 150 µm/ns (km/s) Drive Pressure 40 Mbar (106 atm) 200 Mbar (106 atm)
downstream Upstream preheated
σTs
4 ρous 3/2
SLIDE 3 CLEAR
Radiative shocks are abundant in our universe
Supernova shocks
During propagation
through the star and as it emerges
Supernova ejecta can
develop into a radiative shock
Supernova remnants
can enter a radiative phase
Some accretion
phenomena
3
SN1993J, (Bartel, Science, 2000)
SLIDE 4 CLEAR
Many radiative shock experiments have been performed at HEDP facilities (an abbreviated list)
Driven radiative shock waves
Bouquet, PRL 2004, Koenig, PoP 2006, Reighard, PoP
2006, Doss PoP 2009, Kuranz 2013 and others
Radiative blast waves
Grun, PRL 1991, Edwards PRL 2001, Peterson, 2006,
Hansen, PoP 2006, Moore PRL 2008 and others
Reverse radiative shock waves (relevant to
accretion phenomena)
Facilities include LULI, Omega, Pharos, Janus,
Vulcan, Z machine, Z-beamlet, MAGPIE, NIF (soon) and others
SLIDE 5 CLEAR
Experiments are performed at Omega laser facility
Ten Omega Laser
beams to drive shock
~400 J each, ~4 kJ
total energy
λ = .35 µm, UV light 1 ns square pulse
Produce intensity of
about 1015 W/cm2
Pressure of ~40
Mbars or 40 million atmospheres
Inside the Omega target chamber
Nominal tube Be ! disk 625 µm dia. Xe-filled tube 1200 µm !
Laser
Radiative Shock Target
SLIDE 6 CLEAR
We have performed several experiments exploring the base experiment
We have also used velocity interferometry, streaked optical pyrometry and streaked x-ray radiography to diagnose these experiments
SLIDE 7 CLEAR
We have obtained radiative shock data from 0.5 ns to 30 ns
Differences among shots:
- Laser energy
- Disk Thickness
- Xe pressure
- Tube material (acrylic/
polyimide)
Error bars are the size of the markers
Kuranz, PoP 2013 Kuranz, HEDP 2012 Doss, HEDP 2010
SLIDE 8 CLEAR
We also seek to understand the effect
- f geometry on radiative shocks
Nominal tube Side Views! (diameters are outer diameters) Be ! disk 625 µm dia. Xe-filled tube 1200 µm !
Laser Rear Views 625 x 1200 µm ! elliptical tube Be ! disk Laser Elliptical nozzle tube polyimide! tube acrylic shield Be disk
SLIDE 9 CLEAR
Targets are fabricated at U of Michigan
target stalk polyimide tube gas fill hose diagnostic shield acrylic superstucture
SLIDE 10
CLEAR
Elliptical nozzle is created with machined acrylic
Narrow view Wide view
10 ¡
Acrylic nozzle
SLIDE 11
CLEAR
Radiographic images from an elliptical nozzle target at 26 ns from orthogonal views
SLIDE 12
CLEAR
Radiographic images from an elliptical nozzle target at 26 ns from orthogonal views
SLIDE 13
CLEAR
Radiographic images from an elliptical nozzle target at 26 ns from orthogonal views
SLIDE 14 CLEAR
One quantity of interest is shock location
Shock position varied from 3165 µm to 3818 µm with a mean shock location of 3589 µm and a standard deviation of 164 µm.
SLIDE 15 CLEAR
Variation of experimental parameters
Disk Thickness (µm) Xe pressure (atm) Laser energy (J) Maximum 20.8 1.19 3925 Minimum 20.5 1.06 3850 Mean 20.7 1.12 3886 Standard Deviation 0.1 0.05 20
SLIDE 16
CLEAR
Shock location vs. time for nominal and elliptical tube CRASH experiments
SLIDE 17
CLEAR
We have also compared experimental data with CRASH output
SLIDE 18 CLEAR
Conclusions and future directions
We have completed our Year 5 experiment
exploring a variation in tube geometry
We create driven radiative shocks in the laboratory
with velocities of over 130 km/s!
We have applied a variety of diagnostic techniques
including x-ray radiography, optical pyrometery, and x-ray Thomson scattering
We are using the CRASH code to model the
experiment
This research was supported by the DOE NNSA under the Predictive Science Academic Alliance Program, Stewardship Sciences Academic Alliance and National Laser User Facility program
SLIDE 19
CLEAR
Backup Slides
SLIDE 20 CLEAR
We have observed radiative shocks from 0.5 ns to 30 ns
Shock Breakout data (~0.5 ns)
Diagnostics
Active Shock Breakout (ASBO) Streaked Optical Pyrometer (SOP)
Early-time data (~2 – 7 ns)
Diagnostic Techniques
Gated imaging x-ray radiography Streaked x-ray radiography
Late-time data (~13 – 30 ns)
Diagnostic Technique
Ungated x-ray radiography
Preliminary Variations in Geometry
Elliptical Nozzle Tubes
Be ! disk 625 µm dia. Xe-filled tube Laser
Nominal radiative shock experiment
SLIDE 21 CLEAR
ASBO and SOP can detect the shock breakout from a Be disk
Active Shock
Breakout (ASBO) uses a probe beam to detect the rate of change in the derivative of the
surface
A Streaked Optical
Pyrometer (SOP) passively detects the thermal emission from a surface
21 ¡
Omega ! laser beams
20 µm Be
ASBO ! probe beam ASBO ! and! SOP
SLIDE 22
CLEAR
Shock breakout time is observed on both diagnostics
SOP ASBO Position Position Time Time shock breakout shock breakout
22 ¡
SLIDE 23 CLEAR
We have obtained breakout data from nominally 20 µm Be disks
Systematic error is ± 50 ps
23 ¡
SLIDE 24
CLEAR
We seek to understand the early-time evolution of a driven radiative shock waves
SLIDE 25 CLEAR
We obtained early-time data using gated x-ray radiography
The detector can use a gated camera or streak camera
25 ¡
Drive beams! t = 0 ns 4 - 10 ! backlighter ! beams delayed ! from drive x-ray photons ~5 keV! x-ray source Detector shock
SLIDE 26 CLEAR
We observe these shocks with x-ray radiography from 2 views
The shock is at ~600 µm at 4.5 ns
Kuranz, HEDP (in press)
SLIDE 27
CLEAR
Results from data analysis of streaked and area radiography
Average shock velocity over 130 km/s!
SLIDE 28 CLEAR
The CRASH code simulated the experiment
The CRASH code includes
3D Radiation
Hydrodynamics
Flux-limited multigroup
diffusion
Models laser energy
deposition
t = 4.5 ns Grosskopf Tuesday
SLIDE 29
CLEAR
We obtained late-time radiative shock data using x-ray radiography
Ungated
radiography uses x-ray film as a detector
This technique
requires a large amount of shielding to protect film from unwanted signal t = 13 ns t = 26 ns Doss, HEDP 2010