Published January 7, 2019
| public
Book Section - Chapter
Nitric Oxide Spectroscopic Measurements in a Hypervelocity Stagnation Flow
- Creators
- Yanes, Nelson J.
-
Austin, Joanna M.
Chicago
Abstract
Spatially resolved emission spectra are collected along the stagnation streamline of hypervelocity flow over a circular cylinder. Excitation temperatures are extracted from the NO γ band (A^2Σ^+ - Χ^2Π) emission at downstream locations behind the bow shock. The result is a temperature relaxation profile that quantifies the state of thermal non-equilibrium. Results are compared against a zero-dimensional state-to-state model and a two-temperature, reacting Navier-Stokes simulation. Test gas O_2 mole fraction is varied from 30% to 120% of the air value to examine changes in relaxation profile.
Additional Information
© 2019 American Institute of Aeronautics and Astronautics.Additional details
- Eprint ID
- 97652
- Resolver ID
- CaltechAUTHORS:20190805-134838397
- Created
-
2019-08-07Created from EPrint's datestamp field
- Updated
-
2021-11-16Created from EPrint's last_modified field
- Caltech groups
- GALCIT
- Other Numbering System Name
- AIAA Paper
- Other Numbering System Identifier
- 2019-0794