The amplitude and loudness of conventional N-wave sonic booms vary randomly after propagating through atmospheric turbulence towards the ground. Recent studies have shown that the turbulence effect depends on the amplitude of incoming N-wave. The next generation of supersonic aircraft are designed to produce shaped booms, which are generally lower in amplitude than N-waves and contain shocks with much longer rise times. In this paper, the effect of nonlinearity on shaped sonic booms propagating through turbulence is compared with that for N-waves. Results suggest that nonlinearity may have a negligible impact on loudness variations for shaped signatures, while the impact for N-waves can be significant. Propagation is modeled by solving an augmented KZK propagation equation including the effects of diffraction, thermoviscous absorption, relaxation, nonlinearity, and wind fluctuations.
|Original language||English (US)|
|Journal||Proceedings of Meetings on Acoustics|
|State||Published - Jan 1 2018|
|Event||21st International Symposium on Nonlinear Acoustics, ISNA 2018 - Santa Fe, United States|
Duration: Jul 9 2018 → Jul 13 2018
All Science Journal Classification (ASJC) codes
- Acoustics and Ultrasonics