Cultural advice

The Australian National University acknowledges, celebrates and pays our respects to the Ngunnawal and Ngambri people of the Canberra region and to all First Nations Australians on whose traditional lands we meet and work, and whose cultures are among the oldest continuing cultures in human history.

Aboriginal and Torres Strait Islander peoples are advised that ANU Library collections may include images, names, voices, and other representations of deceased persons.

Material in the collection may contain terms, language or views that reflect the period in which the item was created and may be considered inappropriate today.

A Pump-Probe Laser-Induced Fluorescence Diagnostic for Visualization and Velocimetry in High-Enthalpy Tunnels

Loading...
Thumbnail Image

Date

Authors

Cousens, Samuel
O’byrne, Sean

Journal Title

Journal ISSN

Volume Title

Publisher

American Institute of Aeronautics and Astronautics Inc. (AIAA)

Access Statement

Research Projects

Organizational Units

Journal Issue

Abstract

In this paper we present a relatively inexpensive diagnostic using atomic rubidium that can provide flow visualization and velocimetry in high-enthalpy shock tunnel flows and flames at kHz rates. A two-stage excitation scheme using 5s2 S1/2 → 5p2 P3/2 → 6d2 D3/2 of rubidium is being developed to overcome the issue of fluorescence trapping observed with single-stage excitation from and fluorescence back to the ground state. Alongside this experiment, a model of the fluorescence from both of the excited states in rubidium is being developed. This paper will discuss the diagnostic technique, the rubidium fluorescence model, the proof-of-concept measurements obtained with a rubidium vapor cell, and the current progress of the diagnostic as applied to the T-ADFA free-piston shock tunnel.

Description

Keywords

Citation

Source

Book Title

AIAA AVIATION 2022 Forum

Entity type

Publication

Access Statement

License Rights

Restricted until