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Metal Dimensional Change with Temperature
- Aerospace Standard
- AIR809A
- Reaffirmed
Sector:
Issuing Committee:
Language:
English
Scope
Data are related to the dimensional changes with respect to room temperature and provide accuracy sufficient for use with most aerospace systems. Two basic methods of solution are presented with examples for steady state conditions involving uniform and non-uniform temperature distributions. The answers to the example problems are carried to the fifth place for a comparison of the results between Methods I and II.
Rationale
AIR809A has been reaffirmed to comply with the SAE five-year review policy.
Recommended Content
| Aerospace Material Specification | Room Temperature Tensile Properties of Castings |
| Aerospace Material Specification | Elevated Temperature Tensile Properties of Castings |
| Aerospace Standard | COUPLINGS, CLAMP, GROOVED, V-BAND, 1.75 TO 6.25 FLANGE OD (-65 TO 250 °F) |
Data Sets - Support Documents
No Datasets Available
Issuing Committee
E-25 General Standards for Aerospace and Propulsion Systems
The SAE E-25 General Standards for Aerospace & Propulsion Systems committee addresses aerospace propulsion systems and components. These systems and components include bolts, screws, nuts, washers, studs, rivets, pins, covers, O-rings, brackets, plugs and associated procurement requirements, as well as solid film lubricants and design specifications for screw threads and fastener assembly requirements.
Reference
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