Temperature, Pressure, Velocity, and Water Vapor Mole Fraction Profiles in a Ramjet Combustor using Dual Frequency Comb Spectroscopy and a High Temperature Absorption Database

Fuente: arXiv
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Main Authors: Yun, David, Egbert, Scott C., Malarich, Nathan A., Cole, Ryan K., France, Jacob J., Liu, Jiwen, Rice, Kristin M., Hagenmaier, Mark A., Donbar, Jeffrey M., Hoghooghi, Nazanin, Coburn, Sean C., Rieker, Gregory B.
Format: Preprint
Published: 2024
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author Yun, David
Egbert, Scott C.
Malarich, Nathan A.
Cole, Ryan K.
France, Jacob J.
Liu, Jiwen
Rice, Kristin M.
Hagenmaier, Mark A.
Donbar, Jeffrey M.
Hoghooghi, Nazanin
Coburn, Sean C.
Rieker, Gregory B.
author_facet Yun, David
Egbert, Scott C.
Malarich, Nathan A.
Cole, Ryan K.
France, Jacob J.
Liu, Jiwen
Rice, Kristin M.
Hagenmaier, Mark A.
Donbar, Jeffrey M.
Hoghooghi, Nazanin
Coburn, Sean C.
Rieker, Gregory B.
contents Accurate diagnostics of the combustor region of ramjet engines can improve engine design and create benchmarks for computational fluid dynamics models. Previous works demonstrate that dual frequency comb spectroscopy can provide low uncertainty diagnostics of multiple flow parameters in the non-combusting regions of ramjets. However, the high temperatures present in the combustor present a challenge for broadband spectroscopic absorption models that are used to interpret measurements in these regions. Here, we utilize a new water vapor absorption database created for high temperature water-air mixtures to fit spectra measured in a ground-test ramjet engine with a broadband near-infrared dual comb absorption spectrometer. We extract 2D profiles of pressure, temperature, water mole fraction, and velocity using this new database. We demonstrate that the new database provides the lowest fit residuals compared to other water vapor absorption databases. We compare computational fluid dynamics simulations of the combustor with the measured data to demonstrate that the simulations overpredict heat release and water vapor production.
format Preprint
id arxiv_https___arxiv_org_abs_2403_01380
institution arXiv
publishDate 2024
record_format arxiv
spellingShingle Temperature, Pressure, Velocity, and Water Vapor Mole Fraction Profiles in a Ramjet Combustor using Dual Frequency Comb Spectroscopy and a High Temperature Absorption Database
Yun, David
Egbert, Scott C.
Malarich, Nathan A.
Cole, Ryan K.
France, Jacob J.
Liu, Jiwen
Rice, Kristin M.
Hagenmaier, Mark A.
Donbar, Jeffrey M.
Hoghooghi, Nazanin
Coburn, Sean C.
Rieker, Gregory B.
Fluid Dynamics
Optics
Accurate diagnostics of the combustor region of ramjet engines can improve engine design and create benchmarks for computational fluid dynamics models. Previous works demonstrate that dual frequency comb spectroscopy can provide low uncertainty diagnostics of multiple flow parameters in the non-combusting regions of ramjets. However, the high temperatures present in the combustor present a challenge for broadband spectroscopic absorption models that are used to interpret measurements in these regions. Here, we utilize a new water vapor absorption database created for high temperature water-air mixtures to fit spectra measured in a ground-test ramjet engine with a broadband near-infrared dual comb absorption spectrometer. We extract 2D profiles of pressure, temperature, water mole fraction, and velocity using this new database. We demonstrate that the new database provides the lowest fit residuals compared to other water vapor absorption databases. We compare computational fluid dynamics simulations of the combustor with the measured data to demonstrate that the simulations overpredict heat release and water vapor production.
title Temperature, Pressure, Velocity, and Water Vapor Mole Fraction Profiles in a Ramjet Combustor using Dual Frequency Comb Spectroscopy and a High Temperature Absorption Database
topic Fluid Dynamics
Optics
url https://arxiv.org/abs/2403.01380