TY - JOUR
T1 - Turbulent jet interaction with a long rise-time pressure signature
AU - Ukai, Takahiro
AU - Ohtani, Kiyonobu
AU - Obayashi, Shigeru
N1 - Funding Information:
The authors are grateful to the technical staff of the Institute of Fluid Science, Tohoku University, especially Mr. Toshihiro Ogawa, for the operation of the ballistic range. We also appreciate Mr. Masataka Honna and Mr. Hidenori Ojima for the assistance with the manufacturing. The financial support of the Japan Aerospace Exploration Agency (JAXA) and the Boeing Higher Education Program are also greatly appreciated.
Publisher Copyright:
© 2016 Elsevier Ltd
PY - 2016/12/15
Y1 - 2016/12/15
N2 - A sonic boom signature with a long rise time has the ability to reduce the sonic boom, but it does not necessarily minimize the sonic boom at the ground level because of the real atmospheric turbulence. In this study, an effect of the turbulence on a long rise-time pressure signature was experimentally investigated in a ballistic range facility. To compare the effects of the turbulence on the long and short rise-time pressure signatures, a cone-cylinder projectile that simultaneously produces these pressure signatures was designed. The pressure waves interacted with a turbulent field generated by a circular nozzle. The turbulence effects were evaluated using flow diagnostic techniques: high-speed schlieren photography, a point-diffraction interferometer, and a pressure measurement. In spite of the fact that the long and short rise-time pressure signatures simultaneously travel through the turbulent field, the turbulence effects do not give the same contribution to these overpressures. Regarding the long rise-time pressure signature, the overpressure fluctuation due to the turbulence interaction is almost uniform, and a standard deviation 1.5 times greater than that of the no-turbulence case is observed. By contrast, a short rise-time pressure signature which passed through the same turbulent field is strongly affected by the turbulence. A standard deviation increases by a factor of 14 because of the turbulence interaction. Additionally, there is a non-correlation between the overpressure fluctuations of the long and short rise-time pressure signatures. These results deduce that the length of the rise time is important to the turbulence effects such as the shock focusing/diffracting.
AB - A sonic boom signature with a long rise time has the ability to reduce the sonic boom, but it does not necessarily minimize the sonic boom at the ground level because of the real atmospheric turbulence. In this study, an effect of the turbulence on a long rise-time pressure signature was experimentally investigated in a ballistic range facility. To compare the effects of the turbulence on the long and short rise-time pressure signatures, a cone-cylinder projectile that simultaneously produces these pressure signatures was designed. The pressure waves interacted with a turbulent field generated by a circular nozzle. The turbulence effects were evaluated using flow diagnostic techniques: high-speed schlieren photography, a point-diffraction interferometer, and a pressure measurement. In spite of the fact that the long and short rise-time pressure signatures simultaneously travel through the turbulent field, the turbulence effects do not give the same contribution to these overpressures. Regarding the long rise-time pressure signature, the overpressure fluctuation due to the turbulence interaction is almost uniform, and a standard deviation 1.5 times greater than that of the no-turbulence case is observed. By contrast, a short rise-time pressure signature which passed through the same turbulent field is strongly affected by the turbulence. A standard deviation increases by a factor of 14 because of the turbulence interaction. Additionally, there is a non-correlation between the overpressure fluctuations of the long and short rise-time pressure signatures. These results deduce that the length of the rise time is important to the turbulence effects such as the shock focusing/diffracting.
KW - Ballistic range facility
KW - Low sonic boom signature
KW - Shock-turbulence interaction
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U2 - 10.1016/j.apacoust.2016.07.015
DO - 10.1016/j.apacoust.2016.07.015
M3 - Article
AN - SCOPUS:84980328097
SN - 0003-682X
VL - 114
SP - 179
EP - 190
JO - Applied Acoustics
JF - Applied Acoustics
ER -