Contributions from the National Aerospace Laboratory (NLR), the Aerospace Department of the Delft University of Technology and the Fokker Aircraft Industries are reviewed. The main topics include loads, flight simulation testing procedures, crack initiation and propagation, fatigue tests on notched specimens and panels, residual strength, materials evaluation, fractography, fatigue crack growth, cumulative fatigue damage, F-28, VFW-614, airbus A 300 B, and general investigations. (Author)
Review of Aeronautical Fatigue Investigations in the Netherlands During the Period April 1973 - March 1975
1975
55 pages
Report
No indication
English
Aircraft , Aeronautical engineering , Aircraft structures , Fatigue (Materials) , Netherlands , Airframe materials , Bibliographies , Crack initiation , Crack propagation , Fatigue tests , Flight simulation , Flight tests , Fracture strength , Gust loads , Wing panels , F-28 aircraft , VFW-614 aircraft , A-300 aircraft