TY - GEN
T1 - One-dimensional Interferometric Scattering Velocimetry for High-speed Flows
AU - Krishna, Yedhu
AU - Sekar, Anbarasan
AU - Magnotti, Gaetano
AU - Vaidyanathan, Aravind
N1 - KAUST Repository Item: Exported on 2023-06-06
PY - 2023/5/27
Y1 - 2023/5/27
N2 - Interferometric Rayleigh scattering is an optical diagnostic technique that can be used to measure flow velocity in high-speed flows. Conventionally, the technique collects Rayleigh scattered light from a gas sample and passes it through a Fabry-Perot etalon to generate interference fringes on a camera. When the gas velocity increases, the Doppler shift in the scattered light introduces a shift in the spatial location of fringes and the flow velocity is estimated from this shift by a wavelength calibration of the camera pixels. Recently, the technique was extended to one-dimensional measurements by using a virtually imaged phased array instead of a Fabry-Perot etalon. The current work extends the application of such a one-dimensional interferometric system to seeded high-speed flows which makes the system work with much lower laser power, and discusses the details regarding the optimization of the system for high-speed flow applications.
AB - Interferometric Rayleigh scattering is an optical diagnostic technique that can be used to measure flow velocity in high-speed flows. Conventionally, the technique collects Rayleigh scattered light from a gas sample and passes it through a Fabry-Perot etalon to generate interference fringes on a camera. When the gas velocity increases, the Doppler shift in the scattered light introduces a shift in the spatial location of fringes and the flow velocity is estimated from this shift by a wavelength calibration of the camera pixels. Recently, the technique was extended to one-dimensional measurements by using a virtually imaged phased array instead of a Fabry-Perot etalon. The current work extends the application of such a one-dimensional interferometric system to seeded high-speed flows which makes the system work with much lower laser power, and discusses the details regarding the optimization of the system for high-speed flow applications.
UR - http://hdl.handle.net/10754/692366
UR - https://arc.aiaa.org/doi/10.2514/6.2023-3046
U2 - 10.2514/6.2023-3046
DO - 10.2514/6.2023-3046
M3 - Conference contribution
BT - 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
PB - American Institute of Aeronautics and Astronautics
ER -