Polymer Composites in the Aerospace Industry 2015
DOI: 10.1016/b978-0-85709-523-7.00012-8
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The response of aerospace composites to temperature and humidity

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Cited by 9 publications
(5 citation statements)
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“…Other researchers have also investigated the influence of hygrothermal conditions on damage of carbon/epoxy laminates and reported similar degradation effects. [5,27] The degradation in various mechanical properties of GFRP composites in sea water at different ambient temperature is listed in Table 2.…”
Section: Effect Of Water Absorption On Mechanical Propertiesmentioning
confidence: 99%
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“…Other researchers have also investigated the influence of hygrothermal conditions on damage of carbon/epoxy laminates and reported similar degradation effects. [5,27] The degradation in various mechanical properties of GFRP composites in sea water at different ambient temperature is listed in Table 2.…”
Section: Effect Of Water Absorption On Mechanical Propertiesmentioning
confidence: 99%
“…It is reported that under hot/wet environment, the maximum moisture absorption of GFRP laminates is within the range of 0.75–0.86% which may be achieved at about 250‐day aging. [ 27 ] Immersion in water at high temperature for prolonged period leads to decrease in tensile strength and ductility [ 28 ] and interfacial adhesion [ 10 ] of glass/epoxy composites.…”
Section: Factors Affecting Water Absorptionmentioning
confidence: 99%
“…These results indicate that the tablets were not stable at higher temperature and humidity conditions because increased moisture content can cause a chemical reaction between acid and alkali in effervescent tablets, resulting in premature activation of effervescence reaction and degradation of the product. Additionally, elevated temperature and humidity create a more favorable environment for moisture absorption [80], resulting in increased levels of moisture within the tablet's formulations. Consequently, the friability of tablets in this study decreased.…”
Section: Friabilitymentioning
confidence: 99%
“…Then, the ultimate burst pressure of composite rings can be evaluated by using tensile stress as 25 In which ut and P ut are ultimate tensile stress and ultimate burst pressure, respectively. Also, ID represents inner diameter of the NOL-ring with thickness of t. According to equation (1), the ultimate burst pressure is calculated and plotted in Figure 5. It should be noted that !…”
Section: Internal Burst Pressurementioning
confidence: 99%
“…Satellites and other aeronautical vehicles are exposed to space environment during long-term missions, where cyclic temperature variation is inevitable. 1,2 Due to this, it is very crucial to choose and analyze suitable materials as structural elements. A wealth of available researches suggest that composites can be a perfect choice due to their light weight and reliable thermomechanical features.…”
Section: Introductionmentioning
confidence: 99%