Print Email Facebook Twitter Effect of cooling rate on interlaminar fracture energy and shear strength of APC-2 laminates Title Effect of cooling rate on interlaminar fracture energy and shear strength of APC-2 laminates Author van der Hoeven, W. Institution National Aerospace Laboratory NLR Date 1993-05-31 Abstract The effect of cooling rate on some mechanical properties of APC-2/AS4 composite was investigated over the range between 1 and 70° C/min. Preconsolidated unidirectional laminates were reprocessed in a hot platen press at controlled cooling rates. Double Cantilever Beam specimens and End Notch Flexure specimens were used to determine the mode I and mode II fracture energies, respectively. The interlaminar shear properties were measured using the losupescu shear test method. The results indicated that the shear modulus and the shear strenght tended to decrease slightly with increasing cooling rate. The mode I fracture energy was observed to increase with cooling rate by about 8 per cent within the range investigated. The type of precrack was found to have a significant effect on the mode II fracture energy calculated from the test results. Specimens with mechanically induced precracks yielded fracture energies that were significantly lower than those for specimens with moulded-in precracks. For specimens with mechanically induced precracks the mode II fracture energy was found to increase with cooling rate by about 19 per cent within the range investigated. It is concluded that decreasing the cooling rate below the minimum value specified by the material supplier (10° C/min) will most probably not lead to an abrupt or substantial degradation of the mechanical performance of APC-2. Subject carbon fibre reinforced plasticspeekthermoplastic resinsfracture strengthtemperature effectsstrain energy release ratepolymer matrix compositeslaminatescrack opening displacementcoolingauto claving To reference this document use: http://resolver.tudelft.nl/uuid:07720d39-49ad-4317-889d-91498274b808 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR Technical Publication TP 93288 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1993 National Aerospace Laboratory NLR Files PDF 93288.pdf 36.33 MB Close viewer /islandora/object/uuid:07720d39-49ad-4317-889d-91498274b808/datastream/OBJ/view