![]() |
Aluminum I Beam: 4.00 × 2.311
Home |
Directory |
Career |
News |
Industrial
|
|
![]() ![]()
|
|
Glossary » Beams » Simply Supported » Uniformly Distributed Load » Single Span » Aluminum I Beam » 4.00 × 2.311
Aluminum I Beam |
Single Span
|
Two Equal Spans
|
Three Equal Spans
|
Four Equal Spans
and the maximum normal stress occur at the center of the beam.![]() of aluminum alloys can range from 4061 to 7.614 × 104 psi. The purpose of this page is to give a rough estimation of the load-bearing capacity of this particular beam, rather than a guideline for designing actual building structures. Please check your local building codes for regulatory requirements.
Note: The weight of the beam itself is not included in the calculation.
Additional Information
Related Glossary Pages
Glossary: Beams: Simply Supported: Uniformly Distributed Load: Single Span: Wide Flange Steel I Beam: W14 × 90
Glossary: Beams: Simply Supported: Uniformly Distributed Load: Four Equal Spans: Wide Flange Steel I Beam: W10 × 19 Glossary: Beams: Simply Supported: Uniformly Distributed Load: Two Equal Spans: S Section Steel I Beam: S12 × 40.8 Glossary: Beams: Simply Supported: Uniformly Distributed Load: Four Equal Spans: Wide Flange Steel I Beam: W10 × 112 Glossary: Beams: Simply Supported: Uniformly Distributed Load: Four Equal Spans: Wide Flange Steel I Beam: W12 × 230 Glossary: Beams: Simply Supported: Uniformly Distributed Load: Four Equal Spans: Wide Flange Steel I Beam: W8 × 15 Glossary: Beams: Simply Supported: Uniformly Distributed Load: Two Equal Spans: Wide Flange Steel I Beam: W14 × 53 Glossary: Beams: Simply Supported: Uniformly Distributed Load: Three Equal Spans: Wide Flange Steel I Beam: W10 × 45 Glossary: Beams: Simply Supported: Uniformly Distributed Load: Two Equal Spans: Wide Flange Steel I Beam: W14 × 34 Glossary: Beams: Simply Supported: Uniformly Distributed Load: Four Equal Spans: ALuminum I Beam: 6.00 × 4.030 Related Pages
W Type I-beam search page
Database of standard W Section I-beams with geometric properties.
Engineering Fundamentals: Standard Beams
Database of geometric properties for beams with common cross sections.
Aluminum Ibeams Search Page
Database of standard Aluminum I-beams with geometric properties.
eFunda: Classical Lamination Theory
... the classical lamination theory is only valid for thin laminates (span a and b ... laminate acts as a single lamina with special integrated properties). ...
eFunda: Plate Calculator -- Simply supported rectangular plate ...
This calculator computes the displacement of a simply-supported rectangular plate under a point load.
eFunda: Glossary: Materials: Alloys: Aluminum Alloy: 514.0
It is composed of (in weight percentage) 96.00% Aluminum (Al) and 4.00% Magnesium (Mg). It is usually used in sand casting. ...
Steel S Section I-Beams
Steel S Section I-Beams. ... Check all the I-beams you would like to see properties for and then click GET. ALL. S24 × ___, S20 × ___, S18 × ___, S15 × ___ ...
Critical Load
Consider a long simply-supported column under an external axial load F, ... In general, columns do not always terminate with simply-supported ends. ...
Cantilever Beam Loading Options
Cantilever beams under different loading conditions, such as end load, end moment, intermediate load, uniformly distributed load, triangular load.
eFunda: Glossary: Materials: Alloys: Aluminum Alloy: AA 5050
This calculator computes the displacement of a simply-supported circular plate with free edge under a uniformly distributed load. ...
|
||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||