This report presents, discusses and evaluates the results of many National Aerospace Laboratory NLR investigations into the damage tolerance engineering properties of aerospace aluminum alloys. The investigations cover a period of more than twenty years and represent a considerable source of data. The report is in four parts. Part I comprises chapters 1 and 2, which give an introduction to the significance of aluminum alloys for the aerospace industry and the scope of the report. Parts II and III contain chapters 3-21, which form the main body of the report. Part IV comprises chapters 22 and 23. These provide general conclusions based on the results in Parts II and III, and also recommendations for further work. In Part II, containing chapters 3-15, the engineering properties of new and conventional aluminum alloys are compared, discussed and evaluated. This work commenced in 1969 and ran through to 1990. (Copyright (c) National Aerospace Laboratory NLR The Netherlands.)
Damage Tolerance Engineering Property Evaluation of Aerospace Aluminium Alloys with Emphasis on Fatigue Crack Growth
1995
869 pages
Report
No indication
English
Aircraft , Aerodynamics , Nonferrous Metals & Alloys , Spacecraft Trajectories & Flight Mechanics , Aluminum alloys , Aircraft structures , Fatigue(Mechanics) , Tolerances(Mechanics) , Design , Damage assessment , Aerospace craft , Research programs , Mechanical properties , Fracture tests , Stress corrosion cracking , Strength(Mechanics)
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