Abstract
This paper investigates the use of one-line laser-induced fluorescence (LIF) thermometry of nitric oxide to study hypersonic flows generated by free-piston shock tunnels. This method has several advantages including lower cost, simpler set up, and reduced errors from optical thickness compared to two-line LIF thermometry. However, comparisons between one-line and two-line fluorescence thermometry indicate that the method is unreliable in air flows. The method is used to provide qualitative temperature maps in the separated flow region forward of a blunt fin attached to a flat plate in a Mach 6.4 freestream.
Original language | English |
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DOIs | |
Publication status | Published - 2000 |
Event | 21st Aerodynamic Measurement Technology and Ground Testing Conference 2000 - Denver, CO, United States Duration: 19 Jun 2000 → 22 Jun 2000 |
Conference
Conference | 21st Aerodynamic Measurement Technology and Ground Testing Conference 2000 |
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Country/Territory | United States |
City | Denver, CO |
Period | 19/06/00 → 22/06/00 |