TY - JOUR
T1 - Sonic boom variability due to homogeneous atmospheric turbulence
AU - Yamashita, Hiroshi
AU - Obayashi, Shigeru
N1 - Funding Information:
This study was supported by a grant from the research fellowships of the Japan Society for the Promotion of Science for Young Scientists. The authors wish to thank K. Kusunose of the Ministry of Defense and K. Matsushima of Tohoku University for their invaluable review of and comments on this work. The authors would like to express their gratitude to Y. Naka and Y. Makino of the Japan Aerospace Exploration Agency for their cooperation regarding the loudness calculation on the sonic boom signatures. The authors also wish to acknowledge our colleagues, especially F. K. Nakabayashi, for help in publishing this paper.
PY - 2009
Y1 - 2009
N2 - This study describes the nondeterministic effect of homogeneous atmospheric turbulence on sonic boom propagation. The Sears-Haack body was calculated in three dimensions bycomputational fluid dynamics in inviscid flow (Euler) mode to create the near-field pressure wave. The homogeneous atmospheric turbulence field was represented by the finite sum of discrete Fourier modes based on the von Karman and Pao energy spectrum. The sonic boom signature was then calculated by the modified waveform parameter method, considering a random velocity of homogeneous atmospheric turbulence. The results of this study indicated that atmospheric turbulence has a marked influence on sonic boom overpressure during its propagation to the ground. In comparison to the no-turbulence condition, we found that the sonic boom decreased in 59% of the cases and increased in 41% of the cases. Thus, homogeneous atmospheric turbulence seems to favor a decrease, rather than an increase, in boom overpressure. In addition, we found that turbulence has a small effect on the propagation path from the flight altitude to the ground. Nonetheless, this small change in the propagation path may result in a variability, of the point at which the sonic boom reaches the ground, of up to 1820 ft in the north-south direction (flight direction) and 115 ft in the east-west direction.
AB - This study describes the nondeterministic effect of homogeneous atmospheric turbulence on sonic boom propagation. The Sears-Haack body was calculated in three dimensions bycomputational fluid dynamics in inviscid flow (Euler) mode to create the near-field pressure wave. The homogeneous atmospheric turbulence field was represented by the finite sum of discrete Fourier modes based on the von Karman and Pao energy spectrum. The sonic boom signature was then calculated by the modified waveform parameter method, considering a random velocity of homogeneous atmospheric turbulence. The results of this study indicated that atmospheric turbulence has a marked influence on sonic boom overpressure during its propagation to the ground. In comparison to the no-turbulence condition, we found that the sonic boom decreased in 59% of the cases and increased in 41% of the cases. Thus, homogeneous atmospheric turbulence seems to favor a decrease, rather than an increase, in boom overpressure. In addition, we found that turbulence has a small effect on the propagation path from the flight altitude to the ground. Nonetheless, this small change in the propagation path may result in a variability, of the point at which the sonic boom reaches the ground, of up to 1820 ft in the north-south direction (flight direction) and 115 ft in the east-west direction.
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U2 - 10.2514/1.40215
DO - 10.2514/1.40215
M3 - Article
AN - SCOPUS:73849150195
SN - 0021-8669
VL - 46
SP - 1886
EP - 1893
JO - Journal of Aircraft
JF - Journal of Aircraft
IS - 6
ER -