SAE AIR1751A PDF

SAE AIR1751A PDF

Name:
SAE AIR1751A PDF

Published Date:
08/16/2012

Status:
Active

Description:

Prediction Method for Lateral Attenuation of Airplane Noise During Takeoff and Landing (Stabilized: Aug 2012)

Publisher:
SAE International

Document status:
Active

Format:
Electronic (PDF)

Delivery time:
10 minutes

Delivery time (for Czech version):
200 business days

SKU:
sae-air1751a_1841355

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36.60 €
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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.
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Published : 08/16/2012

History

SAE AIR1751A
Published Date: 08/16/2012
Prediction Method for Lateral Attenuation of Airplane Noise During Takeoff and Landing (Stabilized: Aug 2012)
36.60 €
SAE AIR 1751
Published Date: 03/30/1981
Prediction Method of Lateral Attenuation of Airplane Noise During Takeoff and Landing ( Reaffirmed: 2 Feb 1991 )

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