TY - JOUR
T1 - Mechanics of the influx phase in the jet regurgitant mode of a powered resonance tube
AU - Thethy, Bhavraj
AU - Tairych, David
AU - Edgington-Mitchell, Daniel
PY - 2019/4/1
Y1 - 2019/4/1
N2 - Time-resolved visualisation of shock wave motion within a powered resonant tube (PRT) is presented for the regurgitant mode of operation. Shock position and velocity are measured as functions of both time and space from ultra-high-speed schlieren visualisations. The shock wave velocity is seen to vary across the resonator length for both the incident and reflected waves. Three mechanisms are explored as explanations for the variation in velocity: change in local fluid velocity, variation in shock strength and variations in local temperature. For the incident wave, local fluid velocity and shock strength are extracted from the data and both are demonstrated to contribute to the observed variation, with a non-trivial remainder likely explained by variation in temperature.
AB - Time-resolved visualisation of shock wave motion within a powered resonant tube (PRT) is presented for the regurgitant mode of operation. Shock position and velocity are measured as functions of both time and space from ultra-high-speed schlieren visualisations. The shock wave velocity is seen to vary across the resonator length for both the incident and reflected waves. Three mechanisms are explored as explanations for the variation in velocity: change in local fluid velocity, variation in shock strength and variations in local temperature. For the incident wave, local fluid velocity and shock strength are extracted from the data and both are demonstrated to contribute to the observed variation, with a non-trivial remainder likely explained by variation in temperature.
KW - cavity resonance
KW - Hartmann-Sprenger tube
KW - jet regurgitant mode
KW - powered resonance tube
KW - shock wave velocity
UR - http://www.scopus.com/inward/record.url?scp=85065574791&partnerID=8YFLogxK
U2 - 10.1177/1475472X19840001
DO - 10.1177/1475472X19840001
M3 - Article
AN - SCOPUS:85065574791
SN - 1475-472X
VL - 18
SP - 279
EP - 298
JO - International Journal of Aeroacoustics
JF - International Journal of Aeroacoustics
IS - 2-3
ER -