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Static and fatigue testing bolted, bonded and hybrid step lap joints of thick carbon fibre/epoxy laminates used on aircraft structures

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What this work says

Outgoing claims: the papers this work cites, builds on, or argues with.

inferredcites →https://doi.org/10.1016/0013-7944(89)90165-3openalex-snapshot
An experimental investigation into the effect of impact damage on the compressive strength of step lap joints
inferredcites →https://doi.org/10.1016/0263-8223(95)00071-2openalex-snapshot
Effects of joint geometry and bolt torque on the structural performance of single bolt tension joints in pultruded GRP sheet material
inferredcites →https://doi.org/10.1016/b978-008042699-0/50007-3openalex-snapshot
Fatigue Testing of Generic Bonded Joints
inferredcites →https://doi.org/10.1016/j.compositesb.2015.09.038openalex-snapshot
Experimental and finite element studies of thin bonded and hybrid carbon fibre double lap joints used in aircraft structures
inferredcites →https://doi.org/10.1016/j.compositesb.2016.06.061openalex-snapshot
Experimental and finite element studies of bolted, bonded and hybrid step lap joints of thick carbon fibre/epoxy panels used in aircraft structures
inferredcites →https://doi.org/10.1016/j.compstruct.2004.04.023openalex-snapshot
Evaluation of fatigue characteristics for adhesively-bonded composite stepped lap joint
inferredcites →https://doi.org/10.1016/j.compstruct.2014.11.004openalex-snapshot
Static and fatigue testing thin riveted, bonded and hybrid carbon fiber double lap joints used in aircraft structures
inferredcites →https://doi.org/10.1016/j.engfailanal.2014.07.014openalex-snapshot
Investigation of bolt clamping force on the fatigue life of double lap simple bolted and hybrid (bolted/bonded) joints via experimental and numerical analysis
inferredcites →https://doi.org/10.1016/j.ijadhadh.2004.11.007openalex-snapshot
Theoretical and experimental research into optimal edge taper of bonded repair patches subject to fatigue loadings
inferredcites →https://doi.org/10.1016/s0263-8223(01)00005-8openalex-snapshot
Effects of stacking sequence and clamping force on the bearing strengths of mechanically fastened joints in composite laminates
inferredcites →https://doi.org/10.1243/pime_proc_1995_209_278_02openalex-snapshot
An Engineer'S Viewpoint on Design and Analysis of Aircraft Structural Joints
inferredcites →https://doi.org/10.1520/stp33472sopenalex-snapshot
Further Developments in the Design and Analysis of Adhesive-Bonded Structural Joints
inferredcites →https://doi.org/10.2322/jjsass1969.43.213openalex-snapshot
Composite Materials for Aircraft Structures.
inferredcites →https://doi.org/10.2514/6.2011-7032openalex-snapshot
Durability and Residual Strength Assessment of F/A-18 A-D Wing-Root Stepped-Lap Joint
inferredcites →https://doi.org/10.31399/asm.hb.v21.a0003384openalex-snapshot
Bolted and Bonded Joints
inferredcites →https://doi.org/10.4271/2005-01-3149openalex-snapshot
NASA Heavy Lift Rotorcraft Systems Investigation
inferredcites →https://doi.org/10.5281/zenodo.15414532openalex-snapshot
ANALYSIS AND MEASUREMENT OF SCARF-LAP AND STEP-LAP JOINT REPAIR IN COMPOSITE LAMINATES

What points at this work

Incoming claims: where this work appears in other papers’ reference lists and arguments.

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inferred← citeshttps://doi.org/10.1016/j.compositesb.2016.06.061openalex-snapshot
Experimental and finite element studies of bolted, bonded and hybrid step lap joints of thick carbon fibre/epoxy panels used in aircraft structures
inferred← citeshttps://doi.org/10.1016/j.compositesb.2016.11.048openalex-snapshot
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Revealing the competitive fatigue failure behaviour of CFRP-aluminum two-bolt, double-lap joints
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On the progressive fatigue failure of mechanical composite joints: Numerical simulation and experimental validation
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A novel method for damage analysis of CFRP single-lap bolted, bonded and hybrid joints under compression
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Assembly technology for aeronautical CFRP structures under the collaborative constrains of geometric shape, physical performance and service stability
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