Pressure measurement in supersonic air flow by differential absorptive laser-induced thermal acoustics.
Nonintrusive, off-body flow barometry in Mach 2 airflow has been demonstrated in a large-scale supersonic wind tunnel using seedless laser-induced thermal acoustics (LITA). The static pressure of the gas flow is determined with a novel differential absorption measurement of the ultrasonic sound produced by the LITA pump process. Simultaneously, the streamwise velocity and static gas temperature of the same spatially resolved sample volume were measured with this nonresonant time-averaged LITA technique. Mach number, temperature, and pressure have 0.2%, 0.4%, and 4% rms agreement, respectively, in comparison with known free-stream conditions.
Hart
Roger C
RC
NASA Langley Research Center, Hampton, VA 23681, USA.
Herring
G C
GC
Balla
R Jeffrey
RJ