Affiliation:
1. NASA Langley Research Center
Abstract
A method is presented to acquire self-aligned focusing schlieren (SAFS)
images when the optical axis of the instrument is positioned at a
non-normal incidence angle to the background plane on which the grid
pattern is projected, or to the measurement plane on which gradients
in density are visualized, or both. This is accomplished by applying
the Scheimpflug principle and properly orienting the planes on which
the physical grid pattern and image sensor reside within the
instrument so that focused schlieren images on the measurement plane
can be captured. Focused schlieren images from laboratory tests, where
the background plane and measurement plane were separately and then
simultaneously oriented at non-normal incidence to the instrument’s
optical axis, were acquired with and without the appropriate
Scheimpflug adjustments. The results with the appropriate Scheimpflug
adjustments provided the highest quality focused schlieren images.
However, for the scale of the experiments in this work, it was
determined that the Scheimpflug adjustment to the image sensor
affected focused schlieren image quality more than adjustment to the
grid pattern plane. Based on the results of the initial experiments,
two demonstration tests were performed to highlight the applicability
of the technique in optically constrained environments. In the first
test, relatively good focused schlieren images were acquired using a
curved background plane. In the second test, two synchronized
high-speed (100 kHz) SAFS systems acquired images of a jet flow
with overlapping fields-of-view where their optical axes were at
non-normal incidence to the measurement plane, along which the jet
propagated. The resulting images were then stitched together in
post-processing so that an extended field-of-view could be imaged at a
resolution and framing rate that exceeded that of a single high-speed
SAFS system. In general, the results of this work show that
high-quality focused schlieren images can be obtained with the
background plane and measurement plane oriented over a large range of
angles relative to the SAFS instrument’s optical axis.
Funder
National Aeronautics and Space
Administration
Aeronautics Research Mission
Directorate