Dendrite Arm Spacing of Structural Aircraft Quality D357 Aluminum Alloy Castings, Determination and Acceptance of

Standard [CURRENT]

SAE ARP 1947D:2024-05-09

Dendrite Arm Spacing of Structural Aircraft Quality D357 Aluminum Alloy Castings, Determination and Acceptance of

Publication date
2024-05-09
Original language
English
Pages
8

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Publication date
2024-05-09
Original language
English
Pages
8
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Short description

This document covers the recommended practice for determining the acceptability of the dendrite arm spacing (DAS) of D357-T6 aluminum alloy castings required to have tensile strength not lower than 50 ksi (345 MPa).
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