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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Boron and graphite filament-resin composites tensile and interlaminar shear strengths and Al foil liner cyclic life in cryogenic pressure vessel tests
Tensile strength properties of glass, boron, and graphite filament wound resin composites and liners for cryogenic pressure vessels
Small amplitude linear analysis of combustion instability with finite Mach number flow and acoustic liners
Experimental, and theoretical evaluations of acoustic liners for screech suppression in rocket engines
Hydrogen-oxygen rocket engine used to test acoustic liner with isolated resonators and variable cavity depths
Combustion instability with finite Mach number flow and acoustic liners
Axial and circumferential segmented combustor liners for turbojet engine
Behavior of convergent-divergent nozzles and acoustic liners in three dimensional acoustic fields
Glass, boron and graphite filament wound resin composites and liners for cryogenic pressure vessels
Flow liner eliminates high-cycle fatigue in ducts carrying cryogenic fluids. It is capable of handling two-directional, high-velocity cryogenic liquid flow with a 3-inch axial motion without binding within a 25-inch length.
Theoretical studies and test facility installation for investigating behavior of rocket nozzles and acoustic liners in three dimensional acoustic fields
Frequency responses of supercritical nozzles and acoustic liners
Acoustic liner for controlling combustion instability in rocket engines using ablative chambers
Metal lined glass filament-wound pressure vessel performance at cryogenic temperatures, discussing fibers, resins and liners
F-1 rocket engine acoustic liner, reevaluating damping data for combustion stability improvement
Liners for nitric and hydrofluoric acid tanks show no sign of deterioration after 18 months of continuous use. Each side of each edge of the polypropylene sheets is chamfered, and sheets are welded from both sides with polypropylene filler rod and a special hot-air welding torch.
Shortening transition liner to decrease overall length of ram induction combustor
Behavior of nozzles and acoustic liners in three dimensional acoustic fields