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Using Computational Flow Imaging to Optimize Filtered Rayleigh Scattering Measurements of an Isolator Shock TrainFiltered Rayleigh scattering (FRS) is a laser diagnostic where the intensity of elastically scattered light is measured after it passes through a molecular absorption filter. The filter removes background interference that overwhelms the relatively weak scattering from the gas molecules. However, with a filter, the measured light intensity depends on many of the scattering gas properties, including pressure, density, temperature, and velocity. In this work, CFD simulations of an isolator shock train flow field are input into a physics-based model to predict the values of FRS intensity measurements in a proposed experiment. The goal is to evaluate if a simplistic FRS setup (that utilizes one camera, laser, and absorption filter) can be used to accurately quantify number density despite the fact that the scattered light intensity also depends on other gas properties. It is found that the experimental setup can be optimized such that a linear relationship describes the number density with an average prediction error of 2%. The vast majority of the flow exhibits prediction errors of less than 3%, but small regions of the flow reach up to 11% error. A sensitivity analysis shows that the prediction error increases with the central wavelength of the incident laser light and decreases with the angle between the camera and laser propagation directions. The optimal experimental parameters are chosen based on a compromise between the prediction error, spatial resolution, and the amount of unfiltered light. In the future, the proposed FRS setup will be implemented to acquire new and valuable information on an isolator shock train, a flow field that has been traditionally studied using wall static pressure measurements and path-integrated visualization techniques, such as schlieren and shadowgraphy.


Document ID
20200002705
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Hunt, Robin L.
(NASA Langley Research Center Hampton, VA, United States)
Ground, Cody R.
(NASA Langley Research Center Hampton, VA, United States)
Baurle, Robert A.
(NASA Langley Research Center Hampton, VA, United States)
Danehy, Paul M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
April 20, 2020
Publication Date
August 19, 2019
Subject Category
Aerodynamics
Report/Patent Number
NF1676L-32370
Report Number: NF1676L-32370
Meeting Information
Meeting: 2019 AIAA Propulsion and Energy Forum
Location: Indianapolis, IN
Country: United States
Start Date: August 19, 2019
End Date: August 22, 2019
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
WBS: 725017.02.07.02.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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