Riveting in metal airplane construction. Part III : strength of riveted joints in duralumin (continued) (1930)
NASA Technical Reports Server (NTRS) · leaf 40
N.A-C.A. Technical Memorandum No.598 Fige .111,112,113,114,115 Pig.113 Distribution of stress in strap end. fig.112 Lines of force in a strap end. … fSSO -TV ' 1— Fig.115 Stress Fig.117 Ridge for- distribution Fig.lll Teariag mation at hole edge in strap end stress at criti caused by body of at upper edge. cal section. riTet.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
