SAE AS 5900E:2021

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Standard Test Method for Aerodynamic Acceptance of AMS1424 and AMS1428 Aircraft Deicing/Anti-Icing Fluids

Published By	Publication Date	Number of Pages
SAE	2021-08-19	37

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Categories: 49 - Aircraft and space vehicle engineering, SAE

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This SAE Aerospace Standard (AS) establishes the aerodynamic flow-off requirements and test procedures for AMS1424 Type I and AMS1428 Type II, III, and IV fluids used to deice and/or anti-ice aircraft.

The objective of this standard is to ensure acceptable aerodynamic characteristics of the deicing/anti-icing fluids as they flow off of aircraft lifting and control surfaces during the takeoff ground acceleration and climb. Aerodynamic acceptance of an aircraft ground deicing/anti-icing fluid is based upon the fluid’s boundary layer displacement thickness (BLDT) on a flat plate, measured after experiencing the free stream velocity time history of a representative aircraft takeoff. Acceptability of the fluid is determined by comparing BLDT measurements of the candidate fluid with a datum established from the values of a reference fluid BLDT and the BLDT over the dry (clean) test plate. Testing is carried out in the temperature range at which the fluid, undiluted and diluted, is to be used in airline service.

Published Code

SAE

Published By

SAE International, formerly Society of Automotive Engineers

Publication Date

2021-08-19

Pages Count

Language

English

Descriptors

Wind tunnel tests; Aerodynamics; Test procedures; Aircraft; Test facilities; Aircraft deicing; Humidity; Materials properties; Thermal testing; Test equipment and instrumentation

File Size

3.4 MB

ICS Codes

49 - Aircraft and space vehicle engineering


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SAE AS 5900E:2021

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