作者: L. Molent , R.J. Callinan , R. Jones
DOI: 10.1016/0263-8223(89)90030-5
关键词: Epoxy 、 Reinforcement 、 Cracking 、 Boron 、 Engineering 、 Static testing 、 Wing 、 Stress (mechanics) 、 Structural engineering
摘要: Abstract This paper presents an overview of the structural aspects design and development a local reinforcement designed to lower stresses in region F-111C wing pivot fitting which is prone cracking. The stress analysis, representative specimen testing, thermal analysis full-scale static testing this are summarized.