Abstract
The current interest in hypersonic flows and the growing importance of plasma applications necessitate the development of diagnostics for high-enthalpy flow environments. Reliable and novel experimental data at relevant conditions will drive engineering and modeling efforts forward significantly. This study demonstrates the usage of nanosecond Coherent Anti-Stokes Raman Scattering (CARS) to measure temperature in an atmospheric, high-temperature (> 5500 K) air plasma. The experimental configuration is of interest as the plasma is close to thermodynamic equilibrium and the setup is a test-bed for heat shield materials. The determination of the non-resonant background at such high-temperatures is explored and rotational-vibrational equilibrium temperatures of the N2 ground state are determined via fits of the theory to measured spectra. Results show that the accuracy of the temperature measurements is affected by slow periodic variations in the plasma, causing sampling error. Moreover, depending on the experimental configuration, the measurements can be affected by two-beam interaction, which causes a bias towards lower temperatures, and stimulated Raman pumping, which causes a bias towards higher temperatures. The successful demonstration of CARS at the present conditions, and the exploration of its sensitivities, paves the way towards more complex measurements, e.g. close to interfaces in high-enthalpy plasma flows.
| Original language | English |
|---|---|
| Title of host publication | AIAA SciTech Forum and Exposition, 2023 |
| DOIs | |
| State | Published - 2023 |
| Event | AIAA SciTech Forum and Exposition, 2023 - Orlando, United States Duration: Jan 23 2023 → Jan 27 2023 |
Publication series
| Name | AIAA SciTech Forum and Exposition, 2023 |
|---|
Conference
| Conference | AIAA SciTech Forum and Exposition, 2023 |
|---|---|
| Country/Territory | United States |
| City | Orlando |
| Period | 1/23/23 → 1/27/23 |
Bibliographical note
Publisher Copyright:© 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
Funding
This work was funded by the United States Department of Energy (DOE) and its National Nuclear Security Administration (NNSA). University of Texas personnel are supported by the Department of Energy, National Nuclear Security Administration under Award Number DE-NA0003969. Sandia National Laboratories personnel were supported by DOE/NNSA Science Campaign-6 funding. Sandia National Laboratories is a multimission laboratory managed and operated by the National Technology and Engineering Solutions of Sandia, LLC, a wholly owned subsidiary of Honeywell International, Inc., for the U.S. Department of Energy’s National Nuclear Security Administration under Contract No. DE-NA0003525.
| Funders | Funder number |
|---|---|
| National Nuclear Security Administration | |
| U.S. Department of Energy EPSCoR | DE-NA0003525, DE-NA0003969 |
ASJC Scopus subject areas
- Aerospace Engineering
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