Assembly for Simplified Hi-Res Flow Visualization

instrumentation
Assembly for Simplified Hi-Res Flow Visualization (LAR-TOPS-348)
Self-aligned, single grid projection focusing schlieren imaging system
Overview
Researchers at NASAs Langley Research Center have developed a simple, compact, easy-to-use projection focusing schlieren imaging system optical assembly that leverages a light source, a single physical grid element, and polarization optics to enable hi-res flow visualization. The assembly can simply be mounted in front of a camera to enable focusing schlieren imaging capability. The assembly was designed to drastically reduce the complexity and time required to align a focusing schlieren imaging experiment. Conventional focusing schlieren imaging systems and projection-based analogs require cumbersome grid alignment and peripheral resources to function (e.g., separate source and cutoff grids, projectors, specialized software). NASAs system leverages a single physical grid as both the source and cutoff grid, so the system is self-aligned, compact, does not require specialized software, and costs less than other projection-based alternatives.

The Technology
NASAs single grid, self-aligned focusing schlieren optical assembly is attached to a commercial-off-the-shelf camera. It directs light from the light source through a condenser lens and linear polarizer towards a polarizing beam-splitter where the linear, vertically-polarized component of light is reflected onto the optical axis of the instrument. The light passes through a Ronchi ruling grid, a polarizing prism, and a quarter-wave plate prior to projection from the assembly as right-circularly polarized light. The grid-patterned light (having passed through the Ronchi grid) is directed past the density object onto a retroreflective background that serves as the source grid. Upon reflection off the retroreflective background, the polarization state of light is mirrored. It passes the density object a second time and is then reimaged by the system. Upon encountering the polarizing prism the second time, the light is refracted resulting in a slight offset. This refracted light passes through the Ronchi ruling grid, now serving as the cutoff grid, for a second time before being imaged by the camera. Both small- and large-scale experimental set ups have been evaluated and shown to be capable of fields-of-view of 10 and 300 millimeters respectively. Observed depths of field were found to be comparable to existing systems. Light sources, polarizing prisms, retroreflective materials and lenses can be customized to suit a particular experiment. For example, with a high speed camera and laser light source, the system has collected flow images at a rate of 1MHz.
Raw high-speed images of the shock wave and thermal plume from a spark, imaged at (a) 20 kHz, (b) 100 kHz, (c) 400 kHz, and (d) 1 MHz.
Benefits
  • Easy to use: The single grid design is inherently self-aligned (i.e., precludes the need for fabrication of a source-matched cutoff grid) and the sensitivity is easy to adjust which simplifies set-up saving time (i.e., hours to days) and expands potential user base to those outside of experts in optical diagnostics instrumentation.
  • Compact: The optical assembly is small enough to be mounted like a lens in front of a camera enabling efficient use of space (or room for additional instruments) in cramped experimental environments such as wind tunnels.
  • Vibration insensitive: The self-aligning nature of the instrument prevents grid misalignment issues common to currently employed focusing schlieren instruments
  • High-speed imaging capable: Demonstrated framing rates up to 1 MHZ (dependent on camera and light source used)
  • Modular: System components can be optimized for a given environment, experiment, or cost as the design and method is capable of employing a wide array of light sources, cameras, polarizing prisms, and retroreflective materials.

Applications
  • Aerospace: Flow visualization, aerodynamics and fluid dynamics R&D
  • Thermal Management: instrument to visualize or monitor heat transfer from sensitive electronic devices (e.g., to diagnose thermal issues or determine efficacy of thermal management solutions)
  • Medical: Instrument for contamination control (e.g., mask efficacy, clean room air flows) and diagnostic imaging of air flows or fluid flows
  • Manufacturing: Instrument to visualize gas flow or thermal flow imaging for additive manufacturing or semiconductor manufacturing processes
  • Ventilation: Instrument to visualize air flow from ventilation systems
  • Education: Instrument for primary, secondary, undergraduate or graduate laboratory experiments.
Technology Details

instrumentation
LAR-TOPS-348
LAR-19882-1
11,650,151
Compact, self-aligned focusing schlieren system (June 14, 2021) by inventors Brett F. Bathel and Joshua M. Weisberger in Optics Letters: https://doi.org/10.1364/OL.428011 Development of a Self-Aligned Compact Focusing Schlieren System for NASA Test Facilities (December 29, 2021) presentation at AIAA SCITECH 2022 Forum by inventors Brett F. Bathel and Joshua M. Weisberger: https://arc.aiaa.org/doi/abs/10.2514/6.2022-0560
Similar Results
Image from NASA image library https://images.nasa.gov/details-ACD21-0016-003_F4_P4_4-15_12Hprint.
Digital Projection Focusing Schlieren System
NASAs digital projection focusing schlieren system is attached to a commercial-off-the-shelf camera. For focusing schlieren measurements, it directs light from the light source through a condenser lens and linear polarizer towards a beam-splitter where linear, vertically-polarized component of light is reflected onto the optical axis of the instrument. The light passes through the patterned LCD element, a polarizing prism, and a quarter-wave plate prior to projection from the assembly as left- or right-circularly polarized light. The grid-patterned light (having passed through the LCD element) is directed past the density object onto a retroreflective background (RBG) that serves as the source grid. Upon reflection off the RBG, the polarization state of light is mirrored. It passes the density object a second time and is then reimaged by the system. Upon encountering the polarizing prism the second time, the light is slightly offset. This refracted light passes through the LCD element, now serving as the cutoff grid, for a second time before being imaged by the camera. The LCD element can be programmed to display a variety of grid patterns to enable sensitivity to different density gradients. the color properties of the LCD can be leveraged in combination with multiple colored light sources to enable simultaneous multi-color, multi-technique data collection.
Source is Free NASA Image library
Projected Background-Oriented Schlieren Imaging
The Projected BOS imaging system developed at the NASA Langley Research Center provides a significant advancement over other BOS flow visualization techniques. Specifically, the present BOS imaging method removes the need for a physically patterned retroreflective background within the flow of interest and is therefore insensitive to the changing conditions due to the flow. For example, in a wind tunnel used for aerodynamics testing, there are vibrations and temperature changes that can affect the entire tunnel and anything inside it. Any patterned background within the wind tunnel will be subject to these changing conditions and those effects must be accounted for in the post-processing of the BOS image. This post-processing is not necessary in the Projected BOS process here. In the Projected BOS system, a pattern is projected onto a retroreflective background across the flow of interest (Figure 1). The imaged pattern in this configuration can be made physically (a pattern on a transparent slide) or can be digitally produced on an LCD screen. In this projection scheme, a reference image can be taken at the same time as the signal image, facilitating real-time BOS imaging and the pattern to be changed or optimized during the measurements. Thus far, the Projected BOS imaging technology has been proven to work by visualizing the air flow out of a compressed air canister taken with this new system (Figure 2).
Image from internal NASA presentation developed by inventor and dated May 4, 2020.
Reflection-Reducing Imaging System for Machine Vision Applications
NASAs imaging system is comprised of a small CMOS camera fitted with a C-mount lens affixed to a 3D-printed mount. Light from the high-intensity LED is passed through a lens that both diffuses and collimates the LED output, and this light is coupled onto the cameras optical axis using a 50:50 beam-splitting prism. Use of the collimating/diffusing lens to condition the LED output provides for an illumination source that is of similar diameter to the cameras imaging lens. This is the feature that reduces or eliminates shadows that would otherwise be projected onto the subject plane as a result of refractive index variations in the imaged volume. By coupling the light from the LED unit onto the cameras optical axis, reflections from windows which are often present in wind tunnel facilities to allow for direct views of a test section can be minimized or eliminated when the camera is placed at a small angle of incidence relative to the windows surface. This effect is demonstrated in the image on the bottom left of the page. Eight imaging systems were fabricated and used for capturing background oriented schlieren (BOS) measurements of flow from a heat gun in the 11-by-11-foot test section of the NASA Ames Unitary Plan Wind Tunnel (see test setup on right). Two additional camera systems (not pictured) captured photogrammetry measurements.
Device prototype in use
Optical Head-Mounted Display System for Laser Safety Eyewear
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This star-studded image from NASA's Hubble Space Telescope shows us a portion of Messier 11, an open star cluster in the southern constellation of Scutum (the Shield). Messier 11 is also known as the Wild Duck Cluster, as its brightest stars form a V shape that somewhat resembles a flock of ducks in flight. Messier 11 is one of the richest and most compact open clusters currently known. By investigating the brightest, hottest main sequence stars in the cluster, astronomers estimate that it formed roughly 220 million years ago. Open clusters tend to contain fewer and younger stars than their more compact globular cousins, and Messier 11 is no exception: at its center lie many blue stars, the hottest and youngest of the clusters few thousand stellar residents. The lifespans of open clusters are also relatively short compared to those of globular ones; stars in open clusters are spread farther apart and are thus not as strongly bound to each other by gravity, causing them to be more easily and quickly drawn away by stronger gravitational forces. As a result, Messier 11 is likely to disperse in a few million years as its members are ejected one by one, pulled away by other celestial objects in the vicinity.
Miniaturized Astrometric Alignment Sensor
The Miniaturized Astrometric Alignment Sensor advances satellite capabilities for astrophysical measurements, necessary for formation flying, relative navigation, and virtual telescope capabilities. The sensor is a single assembly consisting of a small, low powered camera assembly. The sensor detects stellar objects from which both stellar and object tracking are performed. The sensors components consist of a low power camera assembly, interchangeable lenses, camera power supply, and image processing software and algorithms. The system functions by searching and identifying objects in the camera's field of view and tracking the objects against a selected star pattern with a central body of interest in the sensor's field of view. The Miniaturized Astrometric Alignment Sensor makes it possible to measure a spacecrafts altitude and orientation with respect to known stellar objects. The instrument takes an image of a patch of sky, identifies the stars in that field of view, and compares the field view with a stored star map. The data is processed with a dedicated processor attached to the instrument to spell out the attitude and orientation of a spacecraft.
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