In the late 1960s and early 1970s research on supersonic aircraft determined that sonic boom noise would penetrate the surface of the ocean. It was assumed that the surface of the air-water interface was perfectly flat. Today, sonic boom noise is once again a topic of interest. The present work concentrates on two-dimensional focusing and defocusing, caused by ocean surface swell, of the penetrating sonic boom waveform. A finite difference algorithm is used to calculate the pressure levels underwater due to a rounded sonic boom waveform interacting with the water interface. Numerical results are consistent with the predictions of known theories involving 1) the existence of pressure disturbances underwater and 2) their penetration depth being a function of the aircraft's speed. These calculations also indicate that 1) the swell of the ocean surface focuses and defocuses the waveform with increasing effect as the ocean wave height increases and 2) the percent change (from a flat ocean interface to a wavy ocean interface) in pressure values due to the swell increases with increasing Mach number.
All Science Journal Classification (ASJC) codes
- Aerospace Engineering