Title: Elastic Stress Waves in candidate Solid Targets for a Neutrino Factory
1Elastic Stress Waves in candidate Solid Targets
for a Neutrino Factory
2Elastic Stress Waves in candidate Solid Targets
for a Neutrino Factory
- Nufact solid target outline and the shockwave
problem
3Elastic Stress Waves in candidate Solid Targets
for a Neutrino Factory
- Nufact solid target outline and the shockwave
problem - Codes used for the study of shockwaves
4Elastic Stress Waves in candidate Solid Targets
for a Neutrino Factory
- Nufact solid target outline and the shockwave
problem - Codes used for the study of shockwaves
- Calculations of proton beam induced stress waves
using the ANSYS FEA Code
5Elastic Stress Waves in candidate Solid Targets
for a Neutrino Factory
- Nufact solid target outline and the shockwave
problem - Codes used for the study of shockwaves
- Calculations of proton beam induced stress waves
using the ANSYS FEA Code - Measurements of proton beam induced stress waves
6Elastic Stress Waves in candidate Solid Targets
for a Neutrino Factory
- Nufact solid target outline and the shockwave
problem - Codes used for the study of shockwaves
- Calculations of proton beam induced stress waves
using the ANSYS FEA Code - Measurements of proton beam induced stress waves
- Experiments with electron beams
7- Schematic outline of a future neutrino factory
8- Schematic of proposed rotating hoop solid target
- Target material needs to pass through capture
solenoid - Could be separate bullets magnetically
levitated
9- Schematic of proposed rotating hoop solid target
- Target material needs to pass through capture
solenoid - Could be separate bullets magnetically
levitated
- Section of target showing temperatures after
single 100 kJ,1 ns - pulse
- Radiation cooled needs to operate at high
temperatures, c.2000ºC
10- Schematic of proposed rotating hoop solid target
- Target material needs to pass through capture
solenoid - Could be separate bullets magnetically
levitated
Shock wave stress intensity contours 4 µs
after100 kJ, 1 ns proton pulse
- Section of target showing temperatures after
single 100 kJ,1 ns - pulse
- Radiation cooled needs to operate at high
temperatures, c.2000ºC
11Pulse power densities for various targets
12Codes used for study of shock waves
- Specialist codes eg used by Fluid Gravity
Engineering Limited Arbitrary
Lagrangian-Eulerian (ALE) codes (developed for
military) - Developed for dynamic e.g. impact problems
- ALE not relevant? Useful for large deformations
where mesh would become highly distorted - Expensive and specialised
13Codes used for study of shock waves
- Specialist codes eg used by Fluid Gravity
Engineering Limited Arbitrary
Lagrangian-Eulerian (ALE) codes (developed for
military) - Developed for dynamic e.g. impact problems
- ALE not relevant? Useful for large deformations
where mesh would become highly distorted - Expensive and specialised
- LS-Dyna
- Uses Explicit Time Integration (ALE method is
included) - suitable for dynamic e.g. Impact problems i.e.
SFma - Should be similar to Fluid Gravity code (older
but material models the same?)
14Codes used for study of shock waves
- Specialist codes eg used by Fluid Gravity
Engineering Limited Arbitrary
Lagrangian-Eulerian (ALE) codes (developed for
military) - Developed for dynamic e.g. impact problems
- ALE not relevant? Useful for large deformations
where mesh would become highly distorted - Expensive and specialised
- LS-Dyna
- Uses Explicit Time Integration (ALE method is
included) - suitable for dynamic e.g. Impact problems i.e.
SFma - Should be similar to Fluid Gravity code (older
but material models the same?) - ANSYS
- Uses Implicit Time Integration
- Suitable for Quasi static problems ie SF0
15Implicit vs Explicit Time Integration
- Explicit Time Integration (used by LS Dyna)
- Central Difference method used
- Accelerations (and stresses) evaluated at time t
- Accelerations -gt velocities -gt displacements
- Small time steps required to maintain stability
- Can solve non-linear problems for non-linear
materials - Best for dynamic problems (SFma)
16Implicit vs Explicit Time Integration
- Implicit Time Integration (used by ANSYS) -
- Finite Element method used
- Average acceleration calculated
- Displacements evaluated at time t?t
- Always stable but small time steps needed to
capture transient response - Non-linear materials can be used to solve static
problems - Can solve non-linear (transient) problems
- but only for linear material properties
- Best for static or quasi static problems (SF0)
17Study by Alec Milne Fluid Gravity Engineering
Limited
- Cylindrical bar 1cm in radius is heated
instantaneously from 300K to 2300K and left to
expand
18Study by Alec Milne, Fluid Gravity Engineering
Limited
The y axis is radius (metres)
19Can ANSYS be used to study proton beam induced
shockwaves?
- Equation of state giving shockwave velocity v.
particle velocity
For tantalum c0 3414 m/s
20Can ANSYS be used to study proton beam induced
shockwaves?
- Equation of state giving shockwave velocity v.
particle velocity
For tantalum c0 3414 m/s Cf ANSYS implicit
wave propagation velocity
ie same as EoS for low particle velocity
21ANSYS benchmark study same conditions as Alec
Milne/FGES study i.e.?T 2000 K
The y axis is radial deflection (metres)
22Comparison between Alec Milne/FGES and ANSYS
results
Alec Milne/ FGES ANSYS
Amplitude of initial radial oscillation 100 µm 120 µm
Radial oscillation period 7.5 µs 8.3 µs
Mean (thermal) expansion 150 µm 160 µm
23ANSYS benchmark study same conditions as Alec
Milne/FGES study - EXCEPT ?T 100 K (not 2000 K)
Surface deflections in 1 cm radius Ta rod over 20
µs after instantaneous uniform temperature jump
of 100 K
24ANSYS benchmark study same conditions as Alec
Milne/FGES study - EXCEPT ?T 100 K (not 2000 K)
Elastic stress waves in 1 cm radius Ta rod over
20 µs after instantaneous (1ns) pulse Stress
(Pa) at centre (purple) and outer radius
(blue)
Surface deflections in 1 cm radius Ta rod over 20
µs after instantaneous uniform temperature jump
of 100 K
25ANSYS benchmark study same conditions as Alec
Milne/FGES study - EXCEPT ?T 100 K (not 2000 K)
Elastic stress waves in 1 cm radius Ta rod over
20 µs after instantaneous (1ns) pulse Stress
(Pa) at centre (purple) and outer radius
(blue)
Surface deflections in 1 cm radius Ta rod over 20
µs after instantaneous uniform temperature jump
of 100 K Cf static case
400 x 106 Pa
26Elastic shock waves in a candidate solid Ta
neutrino factory target
- 10 mm diameter tantalum cylinder
- 10 mm diameter proton beam (parabolic
distribution for simplicity) - 300 J/cc/pulse peak power (Typ. for 4 MW proton
beam depositing 1 MW in target) - Pulse length 1 ns
27Elastic shock waves in a candidate solid Ta
neutrino factory target
Temperature jump after 1 ns pulse (Initial
temperature 2000K )
28Elastic shock waves in a candidate solid Ta
neutrino factory target
Elastic stress waves in 1 cm diameter Ta cylinder
over 10 µs after instantaneous (1ns)
pulse Stress (Pa) at centre (purple) and
outer radius (blue)
29Material model data
- At high temperatures material data is scarce
- Hence, need for experiments to determine material
model data e.g. - Standard flyer-plate surface shock wave
experiment (difficult at high temperatures and
not representative of proton beam loading
conditions) - Scanning electron beam (can achieve stress and
thermal cycling ie fatigue but no shock wave
generated) - Current pulse through wire
- Experiment at ISOLDE (Is it representative? Can
we extract useful data?)
30(No Transcript)
31Elastic shock wave studies for draft ISOLDE
proposal
- 3 mm diameter Ta cylinder
- Beam diameter 1 mm (parabolic distribution for
simplicity) - Peak power deposited 300 J/cc
- Pulse length 4 bunches of 250 ns in 2.4 µs
32Elastic shock wave studies for draft ISOLDE
proposal
Temperature jump after 2.4 µs pulse (Initial
temperature 2000K )
33Elastic shock wave studies for draft ISOLDE
proposal
Temperature profile at centre of cylinder over 4
x 250 ns bunches
34Elastic shock wave studies for draft ISOLDE
proposal
Temperature profile at centre of cylinder over 4
x 250 ns bunches
Radial displacements of target cylinder surface
during and after pulse
35Elastic shock wave studies for draft ISOLDE
proposal
Temperature profile at centre of cylinder over 4
x 250 ns bunches
Elastic stress waves target rod over 5 µs during
and after pulse Stress (Pa) at centre (blue)
outer radius (purple) beam outer radius (red)
36Comparison between Nufact target and ISOLDE test
Peak power density 300 J/cc in both cases
Temperature jump after 2.4 µs pulse (Initial
temperature 2000K )
37Effect of pulse length on shockwave magnitude
38Fibre optic strain gauge system for measuring
stress waves in a proton beam windowNick Simos,
H. Kirk, P. Thieberger (BNL), K. McDonald
(Princeton)
392.4 TP, 100 ns pulse
40- Electron Beam Thermal Cycling Tests at TWI
- CJ Densham, PV Drumm, R Brownsword (RAL)
-
- 175 keV Electron Beam at up to 60 kW beam Power
(CW) - Aims
- High power density electron beam scanned at 4
km/s across foils - Mimics the thermal cycling of tantalum foils to
NF target ?T levels, at a similar T - Lifetime information on candidate target
materials
41Ta foils
Electron Gun
Steel Beam Stop
Aperture plate Optical Transport Window and
bellows
Aperture Plate
Light pipe
To Spectrometer
42Electron Scanning
Upper clamp
Beam Design Path
50 Hz Repetition (100 Hz skip across foils)
Lower guide
Static Load
43Target Foils 25 µm Tantalum
Weight Connectors
44Electron Beam Machine EB1
Electron Beam welder vacuum chamber
CNC table
45(No Transcript)
46Intensity v wavelength of light radiated by Ta
foils
c.500 nm
c.1100 nm
l
47Time profile 20 x 0.5 ms exposures per pulse
(sweep)
128 ms
0 ms
48diamond thermal absorbersJ Butterworth (RAL)
diamond front end crotch absorbers synchrotron
radiation gt 420 W/mm2 heat flux in confined
space