Add to ORKGThe objective of this study was to investigate the feasibility of performing retrogression and reaging (RRA) heat treatments on 2099 aluminum-lithium alloy. The retrogression temperatures were 200-250 A degrees C and retrogression times were 5-60 min. Half of the samples were exposed to a salt fog environment. Interestingly, the samples exposed to salt spray had consistently higher mechanical tensile properties than those which were not exposed
Aluminum alloy 7075 is a useful industrial material thanks to its high strength to weight ratio. How...
The effect of retrogression and reaging heat treatment on corrosion fatigue crack growth behavior on...
Multistep artificial aging treatments coupled with various natural aging times for aluminum lith...
A retrogression and reaging (RRA) treatment was performed on 2195 Al-Li Alloy. The exposure time...
The effect of the retrogression and reaging (RRA) heat treatment on the correlation between microstr...
Aluminum alloy 7075 is a very high strength material and have a wide range application throughout a...
7075 T651 aluminum alloy is frequently used in aircraft applications for its high strength to weight...
Bu tez çalışmasında T6 temper durumunda temin edilen 7075, 7175 ve 6061 kalite alüminyum alaşımlara,...
Retrogression forming and reaging is a new scientific approach to warm forming high strength aluminu...
Retrogression forming and reaging is a new scientific approach to warm forming high strength aluminu...
AbstractA new high strength 2A97 Al-Cu-Li-X alloy was subjected to triple-aging of retrogression and...
The 7075 aluminum alloy was an important structural material in the field of aeronautics and astrona...
Industrial Summary: The 7075 aluminium alloy presents a low stress corrosion cracking strength when ...
Aluminum alloys are widely used in aircraft structural components where light weight, high strength ...
Automotive manufacturers are pursuing technologies, such as lightweighting, that improve vehicle fue...
Aluminum alloy 7075 is a useful industrial material thanks to its high strength to weight ratio. How...
The effect of retrogression and reaging heat treatment on corrosion fatigue crack growth behavior on...
Multistep artificial aging treatments coupled with various natural aging times for aluminum lith...
A retrogression and reaging (RRA) treatment was performed on 2195 Al-Li Alloy. The exposure time...
The effect of the retrogression and reaging (RRA) heat treatment on the correlation between microstr...
Aluminum alloy 7075 is a very high strength material and have a wide range application throughout a...
7075 T651 aluminum alloy is frequently used in aircraft applications for its high strength to weight...
Bu tez çalışmasında T6 temper durumunda temin edilen 7075, 7175 ve 6061 kalite alüminyum alaşımlara,...
Retrogression forming and reaging is a new scientific approach to warm forming high strength aluminu...
Retrogression forming and reaging is a new scientific approach to warm forming high strength aluminu...
AbstractA new high strength 2A97 Al-Cu-Li-X alloy was subjected to triple-aging of retrogression and...
The 7075 aluminum alloy was an important structural material in the field of aeronautics and astrona...
Industrial Summary: The 7075 aluminium alloy presents a low stress corrosion cracking strength when ...
Aluminum alloys are widely used in aircraft structural components where light weight, high strength ...
Automotive manufacturers are pursuing technologies, such as lightweighting, that improve vehicle fue...
Aluminum alloy 7075 is a useful industrial material thanks to its high strength to weight ratio. How...
The effect of retrogression and reaging heat treatment on corrosion fatigue crack growth behavior on...
Multistep artificial aging treatments coupled with various natural aging times for aluminum lith...