TY - GEN
T1 - The measurement of ventilated supercavity interface vibrations
AU - Brungart, Timothy A.
AU - Young, Steven D.
AU - Meyer, Gregory A.
AU - Antonelli, Lynn T.
AU - Winslow, Alia
PY - 2006
Y1 - 2006
N2 - This paper discusses the issues encountered in attempting to perform the first measurements of the interface velocity fluctuations of a ventilated supercavity. A ventilated supercavity is formed and maintained when an upstream cavitator on an undersea vehicle generates a separated flow which is "ventilated," or continuously supplied with gas. This causes the separated flow region or "cavity" to grow and envelop the vehicle. Three laser Doppler vibrometers (LDVs) were used in an attempt to measure the air-water interface vibrations of a ventilated supercavity enveloping a vehicle model in a water tunnel facility. The presence of multiple vibrating surfaces including the tunnel window, model, and interface made determining the velocity spectrum due to the interface alone difficult. The measurements were further complicated by the LDV's electronic noise whose spectrum bears a striking resemblance to that of turbulence velocity fluctuations and, thus, to the spectrum anticipated for the interface. Comparison of the spectra measured with the three LDVs suggests that at least two of the spectra obtained may contain substantial contributions from the ventilated supercavity interface.
AB - This paper discusses the issues encountered in attempting to perform the first measurements of the interface velocity fluctuations of a ventilated supercavity. A ventilated supercavity is formed and maintained when an upstream cavitator on an undersea vehicle generates a separated flow which is "ventilated," or continuously supplied with gas. This causes the separated flow region or "cavity" to grow and envelop the vehicle. Three laser Doppler vibrometers (LDVs) were used in an attempt to measure the air-water interface vibrations of a ventilated supercavity enveloping a vehicle model in a water tunnel facility. The presence of multiple vibrating surfaces including the tunnel window, model, and interface made determining the velocity spectrum due to the interface alone difficult. The measurements were further complicated by the LDV's electronic noise whose spectrum bears a striking resemblance to that of turbulence velocity fluctuations and, thus, to the spectrum anticipated for the interface. Comparison of the spectra measured with the three LDVs suggests that at least two of the spectra obtained may contain substantial contributions from the ventilated supercavity interface.
UR - http://www.scopus.com/inward/record.url?scp=84867969916&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84867969916&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84867969916
SN - 9781604231366
T3 - Institute of Noise Control Engineering of the USA - 35th International Congress and Exposition on Noise Control Engineering, INTER-NOISE 2006
SP - 3397
EP - 3405
BT - Institute of Noise Control Engineering of the USA - 35th International Congress and Exposition on Noise Control Engineering, INTER-NOISE 2006
T2 - 35th International Congress and Exposition on Noise Control Engineering, INTER-NOISE 2006
Y2 - 3 December 2006 through 6 December 2006
ER -