Heterodyne transverse velocimetry for pressure-shear plate impact experiments
Christian Kettenbeil
, Michael Mello
, Moriah Bischann
, and
Guruswami Ravichandran
Citation:
Journal of Applied Physics
123
, 125902 (2018); doi: 10.1063/1.5023007
View online:
https://doi.org/10.1063/1.5023007
View Table of Contents:
http://aip.scitation.org/toc/jap/123/12
Published by the
American Institute of Physics
Heterodyne transverse velocimetry for pressure-shear plate impact
experiments
Christian
Kettenbeil,
a)
Michael
Mello,
Moriah
Bischann,
and Guruswami
Ravichandran
Division of Engineering and Applied Science, California Institute of Technology, 1200 E. California Blvd.,
Pasadena, California 91125, USA
(Received 19 January 2018; accepted 10 March 2018; published online 29 March 2018)
Pressure-shear plate impact experiments have traditionally relied on free space beam interferometers
to measure transverse and normal particle velocities at the rear surface of the target plate. Here, we
present two different interferometry schemes that leverage heterodyne techniques, which enable the
simultaneous measurement of normal and transverse velocities using short-time Fourier transforms.
Both techniques rely on diffracted 1st order beams that are generated by a specular, metallic grating
deposited on the rear surface of the target plate. The diffracted beam photonic Doppler velocimetry
technique interferes each 1st order beam with a reference of slightly higher wavelength to create a
constant carrier frequency at zero particle velocity. The second technique interferes the 1st order
beams with each other and employs an acousto-optic frequency shifter on the
þ
1st order beam to cre-
ate a heterodyne transverse velocimeter. For both interferometer techniques, the 0th order beam is
interfered in a heterodyne photonic Doppler velocimetry arrangement to obtain a measurement of the
normal particle velocity. An overview of both configurations is presented along with a derivation of
the interferometer sensitivities to transverse and normal particle velocities as well as design guidelines
for the optical system. Results from normal impact experiments conducted on Y-cut quartz are pre-
sented as the experimental validation of the two proposed techniques.
Published by AIP Publishing.
https://doi.org/10.1063/1.5023007
I. INTRODUCTION
The measurement of plane waves involving both longi-
tudinal and transverse velocity components is of particular
importance for the study of material strength at high strain
rates (
>
10
4
s
1
) and pressures ranging from hundreds of
MPa to several TPa. These conditions arise in, among others:
pressure-shear plate impact (PSPI) experiments,
1
dynami-
cally loaded anisotropic crystals,
2
,
3
laser-generated shear
waves,
4
and magnetically applied pressure-shear experi-
ments (MAPS).
5
Traditional PSPI experiments rely on the
transverse displacement interferometer (TDI)
2
for the mea-
surement of in-plane displacement histories. Recently, this
technique has been extended to an all fiber-optic configura-
tion.
6
Alternative schemes have leveraged dual VISAR
(Velocity Interferometer System for Any Reflector) arrange-
ments
3
that utilize normal and angled probes to measure
transverse velocity components. The main disadvantage of
this technique is that the fringe constant, as determined by
the etalon delay leg, is set to measure a superposition of both
normal and transverse particle velocities which generally
differ by an order of magnitude. Hence, the dual VISAR
approach cannot realize the full potential of the VISAR inter-
ferometry technique for PSPI experiments.
In recent years, there has been a paradigm shift towards
the application of PDV (photonic Doppler velocimetry) for
normal velocity measurements.
7
Along with the change in
instrumentation came the utilization of robust short-time
Fourier transform analysis techniques that are inherently
more immune to signal noise than previously used phase-
based methods and can therefore tolerate more light loss dur-
ing an experiment. The frequency-based approach is also
largely immune to amplitude modulation of the interferome-
ter signals and does not depend on normalized (amplitude
corrected) fringe records to extract frequency information, as
required when processing a single (unheterodyned) interfer-
ometer signal.
A limitation of “standard” (unheterodyned) PDV is the
inability of the technique to derive temporally resolved mea-
surements of low particle velocities from fringe records or
even partial fringes with correspondingly low signal frequen-
cies. This limitation in temporal resolution leads to inaccura-
cies and signal processing artifacts as demonstrated by the
discrepancy between a synthetic ramp velocity input pulse
and its measured result depicted in Fig.
1(a)
. A heterodyned
interferometer signal exhibits a carrier frequency
f
c
at zero
target velocity as depicted by the ramp wave frequency spec-
trum in Fig.
1(b)
. The increased frequency enables the use
of shorter time windows for the Fourier analysis and thus
provides a high temporal resolution even at low velocities.
While information at low velocities is not always required
for traditional normal plate impact experiments, it is abso-
lutely crucial for measuring transverse velocities in PSPI
experiments, which are typically below 50 m/s.
The main goal of this work is to extend heterodyne PDV
techniques, with their robust frequency-based analysis meth-
ods, to transverse interferometers utilized in PSPI
1
and mag-
netically applied pressure-shear experiments.
5
Two different
approaches were pursued to introduce a carrier frequency
in transverse velocimetry signals. Both techniques rely on
a)
Electronic mail: ckb@caltech.edu
0021-8979/2018/123(12)/125902/14/$30.00
Published by AIP Publishing.
123
, 125902-1
JOURNAL OF APPLIED PHYSICS
123
, 125902 (2018)
diffracted 1st order beams generated by a specular, metallic
grating deposited on the rear surface of the target plate. The
diffracted beam photonic Doppler velocimetry (DPDV) tech-
nique interferes each 1st order beam with a reference laser
adjusted to a slightly higher wavelength. An additional bene-
fit of this transverse velocimeter lies in the independent mea-
sure of the normal velocity record that can be obtained by
decoupling the normal motion from the diffracted order sig-
nals. The second technique, called the heterodyne transverse
velocimeter (HTV), sends the
þ
1st diffracted order through
an acousto-optic frequency shifter to create a carrier fre-
quency upon interference with the –1st order beam. In a sim-
ilar fashion to the transverse displacement interferometer,
2
this approach provides a pure measurement of transverse
motion. A measurement of the normal particle velocity is
obtained from a heterodyne PDV arrangement employing
the reflected 0th order diffracted beam. The strengths and
limitations of each interferometer design are addressed and
the techniques are compared by examining fringe records
obtained from normal impact validation experiments con-
ducted on Y-cut quartz.
II. OPTICAL DESIGN
Collecting diffracted or scattered light at an angle from
the surface normal, to measure in-plane transverse displace-
ments or velocities, poses a set of unique challenges in PSPI
experiments that are not encountered in normal plate impact
experiments. Normal displacement accumulated over the
course of the experiment causes decentering of the diffracted
beams at the receiving fiber-optic probes resulting in a rapid
loss of light intensity. Light loss is further exacerbated by
small tilt angles between the impacted surfaces of the flyer
and target plates. Analyzing the geometrical effects of target
tilt and normal displacement of the target surface can provide
valuable insights into a suitable optical design. The optical
design software Zemax was applied to investigate and quan-
tify light loss due to both of these effects during PSPI experi-
ments. The normal displacement during a PSPI experiment
will depend on the impact velocity, experiment duration, and
material response, resulting in varying optimal designs for
different experiments. However, impact tilts of up to 2 mrad
(0.11
) are considered typical in PSPI experiments and
should lie within the light loss tolerance exhibited by the opti-
cal system.
A. Probe design
Figure
2
shows two optical systems that were investi-
gated for their tolerance to normal displacement and tilt
of the target plate’s rear surface. The calculation of the cou-
pling efficiency requires the computation of an overlap inte-
gral between the electric field that impinges on the fiber-optic
core and the mode that can propagate in the utilized single
mode (SM) fiber. However, many qualitative trends can be
explained by appealing to geometrical optics.
FIG. 1. Frequency spectrum over time
for a ramp velocity input pulse (dashed
line) with inferred velocity for (a)
“standard” and (b) heterodyne PDV.
A Hamming window with a duration
s
¼
15 ns was employed for the fre-
quency analysis.
FIG. 2. Geometrical analysis of light coupling in fiber-optic transverse inter-
ferometers for focused (a) and (b) and collimated (c) and (d) optical designs
subject to normal displacements
D
x
and tilt
a
.
125902-2 Kettenbeil
etal.
J. Appl. Phys.
123
, 125902 (2018)
1. Geometrical analysis of optical system
Figure
2(a)
shows a fiber-optic configuration using focus-
ing probes, which are commonly utilized in normal plate
impact experiments.
8
The advantage of a focused optical sys-
tem is its insensitivity to small rotations of the target rear sur-
face, as highlighted in Fig.
2(b)
. The limitations of using this
approach for transverse measurements become immediately
apparent in Fig.
2(a)
, which highlights how quickly a dif-
fracted or scattered beam is decentered with respect to the
optical axis of the receiving probe upon normal motion of
the target. Figure
2(a)
also indicates that a larger spot size on
the target rear surface, corresp
onding to a longer working dis-
tance
W
, increases the tolerance to normal displacement. The
natural extension of this principle is to introduce a collimated
light system, which is shown in Fig.
2(c)
.Byreducingthe
beam diameter of the source probe, the diffracted beam will
decenter, with respect to the optical axis of the receiving
probe, without a reduction in light intensity at the fiber core
until the decentered beam is vignetted by the edge of the
receiving lens. The disadvantage of a collimated optical sys-
tem is emphasized in Fig.
2(d)
. Any tilt angle
a
of the target
rear surface will introduce a lateral translation of the focused
spot
a
f
from the fiber-optic core, which has a diameter of
8.2
l
m for standard
k
¼
1550 nm wavelength single-mode
fiber. One way to alleviate this concern is to utilize a source
probe lens with a short focal length
f
resulting in a small
source beam diameter. This leads to an enlarged focused spot
size at the focal point of the receiving probe, which is larger
than the fiber-optic core resulting in light coupling even when
the center of the light distribution is displaced laterally by
a
f
.
This approach of increasing the system’s tolerance to tilt
comes at the expense of lower overall coupling efficiency.
However, this does not pose a limitation for the systems pre-
sented here, as light collected by the angled probes is close
to the damage threshold of the photodetectors, which limits
the usable light intensity in the employed interferometer sys-
tems. Another factor that has to be taken into account with
collimated optical systems is that a light beam can only stay
collimated over a finite distance. Assuming Gaussian beam
propagation, the collimation distance corresponds to the con-
focal parameter
b
, given by
9
b
¼
2
z
R
¼
2
px
2
0
k
;
(1)
where
z
R
is the Rayleigh range parameter and
x
0
represents
the beam waist radius. Equation
(1)
highlights the increasing
importance of the Rayleigh range with smaller beam sizes.
The collimated source beam used in the final experimental
configuration has a beam diameter of 280
l
m, which yields a
Rayleigh range
z
R
40 mm, corresponding to an 80 mm col-
limation distance. In order to avoid reductions in coupling
efficiency, the distance between the source and receiving
lens should be kept below this value. In contrast to focusing
systems, collimated designs experience no light loss due to
the depth of field of the employed probe lenses for
W
<
z
R
.
Now that the geometrical effects have been established,
the conflicting nature of the requirements for designs that
accept large tilt angles and have a high tolerance to normal
motion of the target plate becomes evident. A short focal
length of the receiving lens will yield an increased tolerance
to tilt, while a receiving lens with a long focal length will
result in an increased tolerance to decentering from the accu-
mulated normal displacement.
2. Optical simulations
Further progress towards the optical design requires a
more quantitative comparison of several optical configurations.
Optical simulations that propagate electric fields (Zemax
Physical Optics Propagation feature) were carried out to com-
pute the fiber coupling efficiency for varying amounts of nor-
mal displacement and target tilt. The fiber-optic lenses for the
optical simulations were chosen based on typical PDV probes
used for normal plate impact experiments.
8
Geometrical and
optical properties of aspheric lenses with a focal length of
f
¼
1.4 mm, 6.2 mm, and 11 mm were sourced from Thorlabs
and used as input for the optical simulations. Focusing probes
were modeled by a collimator pair of
f
¼
6.2 mm aspheric
lenses for which the spot size at the rear target surface was
minimized by adjusting the spacing of the lenses along the
optical axis.
The coupling efficiencies between the source and the
receiving side probes for two focused and two collimated opti-
cal configurations are shown in Fig.
3
. Focused designs are
characterized by their working distance
W
, whereas collimated
designs are designated by their source and receiving probe lens
focal length
f
. The final coupling efficiency for each receiving
side probe can be obtained by multiplying the results displayed
in Fig.
3
by the diffraction efficiency
I
n
, which depends on the
diffraction grating design and is described in Sec.
II B
.Figure
3(a)
shows, as mentioned in the previous geometrical analysis,
that focusing probes will suffer from a rapid loss of coupling
efficiency upon normal motion of the target. Considering the
immense light loss of the
W
¼
100 mm focused design, it is not
advisable to use working distances at or below this value for
passive receiving probes. Figure
3(a)
confirms that a focused
configuration with a larger working distance
W
is less sensitive
toward normal displacements of the target. As expected, the
light loss designed into the collimated configurations yields a
lower initial coupling efficiency. However, the small relative
change of efficiency with target normal motion makes the col-
limated configuration more suited to transverse interferometry
applications. Typical diagnostic systems can compensate the
lower initial coupling efficiencies with a higher source beam
intensity.
The importance of achieving a low impact tilt during
PSPI experiments with spectrally reflective surfaces is demon-
strated in Fig.
3(b)
. As previously mentioned, especially short
focal length focused configurations offer a higher tolerance to
tilt than collimated systems. However, Fig.
3(b)
confirms the
result of the geometric analysis that using a short focal length
source lens in a collimated system can provide a suitable tilt
tolerance, which can surpass the absolute efficiency of a
W
¼
250 mm focused systems at tilt angles above 1.5 mrad
(0.085
) and provide a much more constant light coupling. As
a result of this analysis, a probe design that incorporates a
f
¼
1.4 mm collimated source lens with a
f
¼
6.2 mm receiving
125902-3 Kettenbeil
etal.
J. Appl. Phys.
123
, 125902 (2018)