Overview of aircraft noise computation methods
Aircraft noise is computed using two primary internationally negotiated methods:
- Certification: Establishes a single noise value per aircraft type at standard reference points around a runway. The primary metric is Effective Perceived Noise Level (EPNL) per ICAO Annex 16, which converts a one-third-octave time history into an EPNdB value using perceived noisiness, tone correction, and duration correction.
- Contour Methods: Predicts the noise impact of a fleet on the surrounding ground area.
- For fixed-wing aircraft, ECAC Doc 29 uses noise-power-distance (NPD) tables and flight path corrections (impedance, lateral attenuation, engine installation, etc.) to create single-event contours.
- For rotorcraft (helicopters), ECAC Doc 32 uses a noise hemisphere model (band levels on a grid of emission angles at a 60m reference distance) combined with spherical spreading, atmospheric absorption, and the Chien-Soroka ground effect to calculate SEL, LASmax, and EPNL contours.