Study and production of polybenzimidazole billets, laminates, and cylinders [PDF]
Mechanical properties and physical, chemical, and thermal tests of polybenzimidazole and carbon fabric laminates for spacecraft thermal ...
Marks, B. S. +2 more
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Warp-Knitted Spacer Fabric Reinforced Syntactic Foam: A Compression Modulus Meso-Mechanics Theoretical Model and Experimental Verification. [PDF]
Polymers (Basel), 2020 Zhi C +6 more
europepmc +1 more source
, 2015 To assist scientists in their pursuit of important research of the subseafloor, the Legacy Borehole Project designed a unique structure that will be lowered to the ocean floor for data collection beneath the ocean floor.
Connelly, Piper +2 more
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Fabrication and Compression Properties of Reinforced Epoxy Syntactic Foam With Basalt Fiber
Advances in Polymer TechnologyDeep-sea equipment is generally made of lightweight and pressure-resistant materials in order to meet the requirements of the actual work. In order to explore marine resources better, it is necessary to research lightweight buoyancy materials for loading
Shuai Cao +12 more
doaj +1 more source
Wind turbine generator rotor blade concepts with low cost potential [PDF]
Four processed for producing blades are examined. Two use filament winding techniques and two involve filling a mold or form to produce all or part of a blade.
Cahill, T. P. +3 more
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Effect of Layer Thickness in Layered Aluminum Matrix Syntactic Foam. [PDF]
Materials (Basel), 2019 Qian C, Liang C, He Z, Ji W.
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The Effect of Microballoon Volume Fraction on the Elastic and Viscoelastic Properties of Hollow Microballoon-Filled Epoxy Composites. [PDF]
Materials (Basel), 2023 Chitrakar R, Hossain MS, Nilufar S.
europepmc +1 more source
Application of composite materials to turbofan engine fan exit guide vanes [PDF]
A program was conducted by NASA with the JT9D engine manufacturer to develop a lightweight, cost effective, composite material fan exit guide vane design having satisfactory structural durability for commerical engine use.
Smith, G. T.
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Advanced manufacturing development of a composite empennage component for L-1011 aircraft. Phase 2: Design and analysis [PDF]
The composite fin design consists of two one-piece cocured covers, two one-piece cocured spars and eleven ribs. The lower ribs are truss ribs with graphite/epoxy caps and aluminum truss members.
Crocker, J. F. +6 more
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Damage Characterization during Compression in a Perlite-Aluminum Syntactic Foam. [PDF]
Materials (Basel), 2019 Kádár C +4 more
europepmc +1 more source