Considering that Al 7475-T7351 plates have good fatigue and crack growth strength and higher fracture toughness than 2024-T351 and others 7XXX alloys, somebody knows why the majors aircraft makers does not use Al 7475-T7351??
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