Abstract
Atmospheric turbulence is known to alter the pressure waveform created by supersonic flight. It is challenging to predict how a particular sonic boom waveform will be affected by a particular atmospheric realization without performing intense atmospheric modeling calculations. This paper attempts to approximate the effects of turbulence as a linear FIR filter. Such a filter is estimated from real sonic boom data measured on the ground and at altitude.
Original language | English (US) |
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Pages (from-to) | 495-503 |
Number of pages | 9 |
Journal | Noise Control Engineering Journal |
Volume | 55 |
Issue number | 6 |
DOIs | |
State | Published - Nov 2007 |
All Science Journal Classification (ASJC) codes
- Building and Construction
- Automotive Engineering
- Aerospace Engineering
- Acoustics and Ultrasonics
- Mechanical Engineering
- Public Health, Environmental and Occupational Health
- Industrial and Manufacturing Engineering