May 24, 2011 #1 conscin Aerospace Joined Jan 24, 2011 Messages 3 Location BR Considering that Al 7475-T351 plates have good fatigue and crack growth strength and higher fracture toughness than 2024 and others 7XXX alloys, anyone knows why the majors aircraft makers does not use that material?? Thanks
Considering that Al 7475-T351 plates have good fatigue and crack growth strength and higher fracture toughness than 2024 and others 7XXX alloys, anyone knows why the majors aircraft makers does not use that material?? Thanks
May 24, 2011 #2 CoryPad Materials Joined Apr 15, 2002 Messages 5,192 Location US Because they use the higher strength overaged versions like 7475-T7651. Use an Internet search for Boeing and 7475 and you will find information. Upvote 0 Downvote
Because they use the higher strength overaged versions like 7475-T7651. Use an Internet search for Boeing and 7475 and you will find information.
May 25, 2011 Thread starter #3 conscin Aerospace Joined Jan 24, 2011 Messages 3 Location BR where you read 7475-T351...please understand 7475-T7351... Upvote 0 Downvote