2016
DOI: 10.1007/s10443-016-9522-3
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Thermoelasticity of a Fabric Membrane Composite for the Stratospheric Airship Envelope Based on Multiscale Models

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Cited by 11 publications
(10 citation statements)
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“…Zhang et al [ 80 ] performed research on the stress-relaxation behaviors of PTFE coated fabrics under temperatures from 23 °C to 70 °C. Meng et al [ 81 ] examined thermal distribution and deformation of coated woven fabrics. Yu et al [ 82 ] studied the mechanical properties of polyvinyl chloride PVC-coated woven fabric exposure to temperature ranges from 20 °C to 170 °C under the uniaxial tensile test.…”
Section: Introductionmentioning
confidence: 99%
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“…Zhang et al [ 80 ] performed research on the stress-relaxation behaviors of PTFE coated fabrics under temperatures from 23 °C to 70 °C. Meng et al [ 81 ] examined thermal distribution and deformation of coated woven fabrics. Yu et al [ 82 ] studied the mechanical properties of polyvinyl chloride PVC-coated woven fabric exposure to temperature ranges from 20 °C to 170 °C under the uniaxial tensile test.…”
Section: Introductionmentioning
confidence: 99%
“…Ambroziak and Kłosowski [78] identify mechanical and thermal properties of PVC-coated polyester fabrics in the range of temperature form −30 • C to +70 • C. Jabbari et al [79] described the thermal degradation, effect of aerogel-content, thermal insulating properties, surface characteristics, and tensile properties of polyester fabrics. Zhang et al [80] performed research on the stress-relaxation behaviors of PTFE coated fabrics under temperatures from 23 • C to 70 • C. Meng et al [81] examined thermal distribution and deformation of coated woven fabrics. Yu et al [82] studied the mechanical properties of polyvinyl chloride PVC-coated woven fabric exposure to temperature ranges from 20 • C to 170 • C under the uniaxial tensile test.…”
Section: Introductionmentioning
confidence: 99%
“…The envelope materials for aerostat must have low density, high strength, excellent weathering, low helium permeability, good stitching process, and easy repair, among other features (Schäfer et al, 2002;Kang et al, 2006;Komatsu et al, 2003), which are of vital significance due to their complex, changeable, and even harsh working conditions (Cicerone, 1987;Caldwell and Flint, 1994;Wrobel et al, 2011). In addition to the application efficiency of the aerostat containing floating height and continuous flight time, the payload and the lifetime directly depend on the properties of the envelope materials (Meng et al, 2016;Meng et al, 2017).…”
Section: Introductionmentioning
confidence: 99%
“…To satisfy the these requirements, envelope materials for aerostat are laminates designed, typically including heatsealing layer, load-carrying layer made of fabric, gasbarrier layer, weathering layer, and adhesive layers (Schäfer et al, 2002;Meng et al, 2017;Vallabh et al, 2021), as shown in Figure 1. The functional load-carrying layer, usually woven from aromatic polyamide (Vectran), polyester, polyethylene, and poly-pphenylenebenzobisthiazole fiber, provides the strength of the whole envelope materials to bear the load, as well as the pressure difference between the inside and outside of aerostat (Komatsu et al, 2003;Zhai and Euler, 2005;Nakadate et al, 2009).…”
Section: Introductionmentioning
confidence: 99%
“…Zhang 52 carried out a series of uniaxial tensile tests to study the tensile performances of the specimens in 11 in-plane directions and six tensile rates. Meng et al 53 described the thermal distribution and the deformation of the envelope material in different temperatures. Meng et al 54 The aim of this research is to determine the longterm mechanical properties under uniaxial tensile tests of the Precontraint 1202 S2 back PVDF polyestercoated fabrics.…”
Section: Introductionmentioning
confidence: 99%