Print Email Facebook Twitter Residual strength of bonded stiffened panels: prediction and experimental verification Title Residual strength of bonded stiffened panels: prediction and experimental verification Author Vlieger, H. Institution National Aerospace Laboratory NLR Date 1983-05-31 Abstract This report presents results of residual strength calculations, carried out on cracked panel configurations of various designs and provided with bonded stiffeners. The calculations were carried out using the computer program BOND. The results of these calculations are compared with results of residual strength tests, performed on panels of similar design. It turns out that the calculation results generally compare well but in some cases are slightly unconservative, depending on panel configuration and material combination of sheet and stiffeners. A description of the computer program BOND is given also. Subject adhesive bondingaircraft construction materialsaluminium alloyscomputer programscrack arrestdamage tolerancefracture strengthpanelsprovingresidual strengthstiffeningstress intensity factorstolerances (mechanics)toughness To reference this document use: http://resolver.tudelft.nl/uuid:511da5e8-a513-4b8b-90e5-a1f5aa9af751 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR 83066 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1983 National Aerospace Laboratory NLR Files PDF NLR_TR_83066_U.pdf 43.41 MB Close viewer /islandora/object/uuid:511da5e8-a513-4b8b-90e5-a1f5aa9af751/datastream/OBJ/view