Pressure and Imaging Diagnostics
Piezoelectric pressure transducers are flush-mounted along the wall of the
shock tube for determining shock speed and for triggering the pulsed laser for
imaging. There are two types of imaging used in the shock tube,
through-field imaging (shadowgraphy and Schlieren) and laser sheet
imaging. An example of the shadowgraphy setup is shown below.
The laser is pulsed at a preset delay time based on the shock strength to
image the interface through the test section. The laser, optics and camera
are supported by a vibration isolation table. The pulsed laser is steered
through a series of mirror, expanded, and then collimated and goes through the
test section onto the screen. The screen is imaged with the CCD camera and
then stored on a computer. With through-field imaging density gradients
(with schlieren) or the gradient of a density gradient (shadowgraphy) appear as
dark areas on the screen. Thus, a planar shock being a thin steep density
gradient appears as a flat line on the screen. This technique also
captures a Richtmyer-Meshkov unstable interface as the interface itself is a
density gradient between two gases. Typically a CCD camera with a 1024x1024 pixel array is used to capture a high resolution image.
The laser sheet imaging setup is shown to the right. In the schematic
there are actually two laser sheets shown, one in the interface section and one
in the test section. The retractable sine plate is shown in the interface
section. For this experiment, the initial conditions are imaged real time
with a CCD camera (either 256x256 or 532x516
pixel array) framing at 100-200 frames per second. The argon ion laser
beam is steered with mirrors for a 488 nm wavelength and enters through a port in the side of the interface section and
illuminates a 2D slice of the interface at the center of the square
cross-section. The camera catches 10-200 frames of the developing interface
(depending on the gas pair used) before the shock wave accelerates the interface
down to into the test section. When the interface is in the test section, the
Nd:Yag laser is triggered and emits a laser pulse that enters the shock tube
through a window in the bottom flange. This laser pulse is
steered with mirrors for a 532 nm wavelength and the test section camera has a
532 nm filter to keep any stray reflections from the other laser from being
imaged on the CCD. Unlike in through-field imaging where density
gradients are seen, in planar imaging it is necessary to scatter light from the
interface into the CCD camera for visualization. Light scattering can
occur off the molecular species (Rayleigh scattering, a weak signal) or by
seeding one of the gases with smoke or a fluorescing molecule.
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