• SAE AIR6297

SAE AIR6297

  • Method to Calculate Behind Start of Takeoff Roll Noise Level Adjustments
  • standard by SAE International, 07/06/2017
  • Category: SAE

$81.00 $41.00

SAE AIR6297 describes a method to calculate noise level adjustments at locations behind an airplane (described by an angular offset or directivity) at the start of takeoff roll (SOTR). This method is derived from empirical data from jet aircraft (circa 2004), most of which are configured with wing-mounted engines with high by-pass ratios (Lau, et al., 2012). Methods are also described which apply to modern turboprop aricraft.
Calculations of other propagation-related adjustments required for aircraft noise prediction models are described in AIR1845A, ARP5534, ARP866A, and AIR5662.
PDF

All of our standards document are available in PDF (Portable Document Format), an electronic, downloadable format.You will be able to download the file in your account downloads.

Multi-User Access

After purchasing, you have the ability to assign each license to a specific user.

Printable

At any time, you are permitted to make printed copies for your and your members' reference use.

SAE AMSQQA250/12A

SAE AMSQQA250/12A

Aluminum Alloy 7075, Plate and Sheet (Stabilized: Dec 2013)..

$41.00 $81.00

SAE AMSQQA250/29A

SAE AMSQQA250/29A

Aluminum Alloy 2124, Plate (Stabilized: Dec 2013)..

$41.00 $81.00

SAE AMSQQA250/30A

SAE AMSQQA250/30A

Aluminum Alloy 2219, Plate and Sheet (Stabilized: Dec 2013)..

$41.00 $81.00

SAE AMS2404G

SAE AMS2404G

Plating, Electroless Nickel..

$41.00 $81.00