SAE ARP 5903:2015-06-01

This document provides information, guidelines, and practices for the application, use, and administration of two-dimensional and three-dimensional droplet impingement and ice accretion computer codes. The codes provide computational simulations of inflight icing that predict droplet trajectory, water loading, and ice accretion on aircraft components. These ice accretion characteristics are used during the aircraft design and certification process.

Author	SAE
Editor	SAE
Document type	Standard
Format	File
Confirmation date	2015-06-01
ICS	49.045 : Structure and structure elements
Number of pages	88
Set	AEROPAKS10U-10
Year	2015
Document history
Country	USA
Keyword	SAE 5903;SAE ARP5903;SAE ARP5903;SAE ARP 5903