Towards the fastenerless composite design

Composites Part A: Applied Science and Manufacturing

Volumn 27, Issue 10, 1996, Pages 915-920

  Van Rijn, L P V M ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

Adhesive bonding; Composite aircraft; Fastenerless design

Indexed keywords

ADHESIVE JOINTS; ADHESIVES; BONDING; CARBON FIBER REINFORCED PLASTICS; COMPOSITE MATERIALS; FASTENERS; FUSELAGES; LOADS (FORCES); PRESSURIZATION; SHEAR STRESS; STRESS CONCENTRATION;

ADHESIVE BONDING; COMPOSITE AIRCRAFT; FASTENERLESS DESIGN; FUSELAGE JOINT; LOAD TRANSFER; PRESSURISATION LOADS;

AIRCRAFT MANUFACTURE;

EID: 0030377676     PISSN: 1359835X     EISSN: None     Source Type: Journal    
DOI: 10.1016/1359-835X(96)00009-7     Document Type: Article

References (5)

1. de Jong, Th., Beukers, A. and Vogelsang, L.B., Weight reduction as an added benefit. In 'Fatigue of Aircraft Materials', Proceedings of the specialists conference dedicated to the 65th birthday of Professor J. Schijve, Delft University Press, 1992
2. Volkersen, O., Die Schubkraftverteiling in Leim, niet und Bolzenverbindingen. Energie und Technik 1953, 3, 68; 1953, 5, 106; 1953, 7, 41
3. Volkersen, O., Die Schubkraftverteiling in Leim, niet und Bolzenverbindingen. Energie und Technik 1953, 3, 68; 1953, 5, 106; 1953, 7, 41
4. Volkersen, O., Die Schubkraftverteiling in Leim, niet und Bolzenverbindingen. Energie und Technik 1953, 3, 68; 1953, 5, 106; 1953, 7, 41
5. Engineering Science Data Unit. Inelastic Shear Stresses and Strains in the Adhesives Bonding Lap Joints Loaded in Tension or Shear, Data Item 79016, 1979