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AL-P2618A-T6511 | EN AW-2618A Material Datasheet

Material Standard Values
Material Models for Simulation

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Material Description

Material Number	Material Number (single)	Standard	Standard Status	Country
2618A-T6511 (DIN EN 3553 : 2006-10)	EN AW-2618A	DIN EN 3553 : 2006-10	Valid	Germany	1)
1) Remark: Aluminum alloy AL-P2618A-T6511 extruded bars and sections up to 160 mm for high loaded aerospace parts up to 300 °C.

Chemical Composition

Cu [%]	Fe [%]	Mg [%]	Mn [%]	Ni [%]	Si [%]	Ti [%]	Zn [%]	Ti+Zr [%]
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Mechanical Properties

Semi-finished Product	Condition	Nominal Size [mm]	Temperature [°C]	Specimen Direction	Tensile Strength [MPa]	Yield Strength (0.2% offset) [MPa]	Elongation A [%]	Elongation A50 [%]	Hardness HB \| HBW
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Physical Properties

Condition	Temperature [°C]	Density [g/cm³]	Young's Modulus [GPa]	Mean Coefficient of Thermal Expansion [10^-6*K^-1]	Thermal Conductivity [W/(m*K)]	Electric Conductivity [MS/m]
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Heat Treatment

Heat Treatment	Step	Temperature [°C]	Holding Time [h]	Medium
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Cross Reference

Material Name	Country	Standard
2618	China	GB/T 3880
EN AW-Al Cu2Mg1,5Ni	Europe	EN 573-3
DTD 5014	Great Britain
AlCu2Mg1,5Ni	International	ISO 209-1
AK4-1ch	Russia	GOST 4784	1)
АК4-1ч	Russia	ГОСТ 4784	1)
EN AW-2618A	Spain	UNE 38320
A92618	USA	UNS
AlCu2MgNi	Germany	WL 3.1924-2
3.1924	Germany	WL 3.1924-2
EN 3553 K	Europe	EN 3553
EN 3553 U	Europe	EN 3553
1) Source: GOST 4784-97

Producer/Supplier/Trade names

Tradename	Supplier
EN AW-2618A	AMAG Austria Metall AG, Braunau-Ranshofen
2618A	AUBERT & DUVAL Deutschland GmbH, München
AL-EN AW-2618A	Batz+Burgel GmbH & Co. KG, Friedberg
AlCu2Mg1,5Ni	Imet Industriemetall Handelsgesellschaft mbH, Hamburg
2618A	Kaiser Aluminum Corporation, Lake Forest
2618A	KASTENS & KNAUER GmbH & Co. INTERNATIONAL KG, Lilienthal
2618A	Novelis AG, Koblenz
AN40.78	OTTO FUCHS KG, Meinerzhagen

Material Compliance

REACh	RoHS
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Linear-elastic

Temperature [°C]	Young's modulus [GPa]	Bulk modulus [GPa]	Shear modulus [GPa]	Poisson's ratio
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Alternating stress

Temperature [°C]	Stress ratio	Mean stress [MPa]	Alternating stress [MPa]	Cycles
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Yield strength

Temperature [°C]	0.1% Proof strength [MPa]	0.2% Proof strength [MPa]	Yield strength [MPa]
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Density

Temperature [°C]	Density [g/cm³]
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Tensile strength

Temperature [°C]	Tensile strength [MPa]
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Thermal conductivity

Temperature [°C]	Thermal conductivity [W/(m*K)]
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Classification

WIAM Material	Treatment	Semi-finished product	Dimension [mm]	Load type	Failure criteria	Rolling direction	Maximum stress [MPa]	Strain at maximum stress [%]	Source description
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Designation

Designation	Material number	Source
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Yield strength

Temperature [°C]	0.1% Proof strength [MPa]	0.2% Proof strength [MPa]	Yield strength [MPa]
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Tensile strength

Temperature [°C]	Tensile strength [MPa]
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Classification

WIAM Material	Treatment	Semi-finished product	Dimension [mm]	Load type	Failure criteria	Rolling direction	Maximum stress [MPa]	Strain at maximum stress [%]	Source description
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Yield strength

Temperature [°C]	0.1% Proof strength [MPa]	0.2% Proof strength [MPa]	Yield strength [MPa]
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Tensile strength

Temperature [°C]	Tensile strength [MPa]
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Classification

WIAM Material	Treatment	Semi-finished product	Dimension [mm]	Load type	Failure criteria	Rolling direction	Maximum stress [MPa]	Strain at maximum stress [%]	Source description
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Yield strength

Temperature [°C]	0.1% Proof strength [MPa]	0.2% Proof strength [MPa]	Yield strength [MPa]
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Tensile strength

Temperature [°C]	Tensile strength [MPa]
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Classification

WIAM Material	Treatment	Semi-finished product	Dimension [mm]	Load type	Failure criteria	Rolling direction	Maximum stress [MPa]	Strain at maximum stress [%]	Source description
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AL-P2618A-T6511 | EN AW-2618A Material Datasheet

Material Standard Values

Material Models for Simulation

Material Description

Chemical Composition

Mechanical Properties

Physical Properties

Heat Treatment

Cross Reference

Producer/Supplier/Trade names

Material Compliance

AL-P2618A-T6511 (2618A-T6511; DIN EN 3553 : 2006-10)

Linear-elastic

Alternating stress

Yield strength

Density

Tensile strength

Thermal conductivity

Classification

Designation

AL-P2618A-T6511 (T6511 (solution heat-treated, stress-relieved by stretching a controlled amount and then artificially aged; minor straightening is allowed after stretching); rod; 0.000-10.000mm)

Yield strength

Tensile strength

Classification

AL-P2618A-T6511 (T6511 (solution heat-treated, stress-relieved by stretching a controlled amount and then artificially aged; minor straightening is allowed after stretching); rod; 10.000-100.000mm)

Yield strength

Tensile strength

Classification

AL-P2618A-T6511 (T6511 (solution heat-treated, stress-relieved by stretching a controlled amount and then artificially aged; minor straightening is allowed after stretching); rod; 100.000-160.000mm)

Yield strength

Tensile strength

Classification