SAE AIR1751

Prediction Method of Lateral Attenuation of Airplane Noise During Takeoff and Landing.

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Standard:
  • AIR1751
Reaffirmed:
  • 1991-02-01
Revised:
  • 1981-06-01
Revision:
  • Historical. Access the latest revision: AIR1751A
Issuing:
  • A-21 Aircraft Noise Measure Noise Aviation Emission Modeling
Scope:

The SAE A-21 Committee on Aircraft Noise undertook in 1979 the development of a uniform and consistent method for the prediction of lateral attenuation. The project was divided into two phases: (1) A short-term phase in which correlations of flight data were made using frequency-weighted and time-integrated measures of the noise, such as Effective Perceived Noise Level (EPNL) and Sound Exposure Level (SEL), see Appendix A; and (2) A long-term phase in which the effects of various sound-propagation phenomena would include ground reflection effects, refraction effects, and airplane shielding effects, as well as other ground and engine/airplane installation effects. This Aerospace Information Report is directed to the short-term phase in order to produce an interim prediction method as soon as possible.

History:
StandardPublishedRevisionStatus
AIR1751A2012-08-16LatestStabilized
AIR17511981-06-01HistoricalReaffirmed
AKA:
  • SAE AIR 1751
Sector:
  • Aerospace
Topic:
  • Landing gear
  • Noise

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