Hypersonic N₂ boundary layer flow velocity profile measurements using FLEET

Authors

Jonathan L. Hill, Air Force Institute of Technology
Paul S. Hsu, Spectral Energies LLC
Naibo Jiang, Spectral Energies LLC
Stephen W. Grib, Spectral Energies LLC
Sukesh Roy, Spectral Energies LLC
Matthew Borg, Air Force Research Laboratory
Levi M. Thomas, Air Force Institute of Technology
Mark F. Reeder, Air Force Institute of TechnologyFollow
Stephen A. Schumaker, Air Force Research Laboratory

Document Type

Article

Publication Date

5-2021

Abstract

Excerpt: Femtosecond laser electronic excitation tagging (FLEET) velocimetry was used in the boundary layer of an ogive-cylinder model in a Mach-6 Ludwieg tube. © OSA.

Comments

© 2021 Optical Society of America. One print or electronic copy may be made for personal use only. Systematic reproduction and distribution, duplication of any material in this paper for a fee or for commercial purposes, or modifications of the content of this paper are prohibited.

The "Link to Full Text" on this page opens or saves the CHORUS-furnished accepted manuscript (postprint) version of the article.

The published version of record is a subscription article in volume 60 of Applied Optics, as cited below.

Plain-text title: Hypersonic N2 boundary layer flow velocity profile measurements using FLEET

DOI

10.1364/AO.417470

Source Publication

Applied Optics

Recommended Citation

Jonathan L. Hill, Paul S. Hsu, Naibo Jiang, Stephen W. Grib, Sukesh Roy, Matthew Borg, Levi Thomas, Mark Reeder, and Stephen A. Schumaker, "Hypersonic N2 boundary layer flow velocity profile measurements using FLEET," Appl. Opt. 60, C38-C46 (2021)