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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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Ground testing of a 1% gravo-aeroelastically scaled additively-manufactured wind turbine blade with bio-inspired structural design
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Material and Structural Design of Novel Binder Systems for High-Energy, High-Power Lithium-Ion Batteries
Not Available
Transition-Metal-Incorporated Aluminum Oxide Thin Films: Toward Electronic Structure Design in Amorphous Mixed-Metal Oxides
Abstract not provided
2D Carbon Phosphide for Trapping Sulfur in Rechargeable Li–S Batteries: Structure Design and Interfacial Chemistry
Not provided.
Hierarchical structural design for fracture resistance in the shell of the pteropod Clio pyramidata
Abstract not provided
Guide RNA structure design enables combinatorial CRISPRa programs for biosynthetic profiling
Not Available
Optimizing the thermoelectric performance of low-temperature SnSe compounds by electronic structure design
Figure-of-merit factor ZT depending on hope-carrier density for single and polycrystal SnSe compounds at T = 675 K.
Xiang et al. Reply: Towards Direct-Gap Silicon Phases by the Inverse Band Structure Design Approach
Abstract not provided
Effect of Epitaxial-Structure Design and Growth Parameters on the Characteristics of Metamorphic Lasers of the 1.46-μm Optical Range Based on Quantum Dots Grown on GaAs Substrates
The characteristics of lasers of the 1.44–1.46-μm optical range grown on GaAs substrates using a metamorphic buffer are studied. The active region of the laser contains 10 rows of InAs/In{sub 0.4}Ga{sub 0.6}As/In{sub 0.2}Ga{sub 0.8}As quantum dots. It is shown that the use of special selective high-temperature annealing along with the application of short-period In{sub 0.2}Ga{sub 0.8}As/In{sub 0.2}Al{sub 0.3}Ga{sub 0.5}As short-period superlattices makes it possible to substantially decrease the density of threading dislocations in the active region. A threshold current density of 1300 A cm{sup –2}, external differential quantum efficiency of 38%, and maximal pulsed-mode output power of 13 W are attained for a laser with a broad area 3 mm in length.
Super-Cell Random APproximates(SCRAPs): A Multicomponent Alloy Structure Design Tool
A novel Hybrid CUCKOO SEARCH determines combinatorial global optimum SCRAPs for specified point and pair correlations in high-entropy alloys having proper distributions.
Improved Structural Design and CO 2 Capture of Porous Hydroxy-Rich Polymeric Organic Frameworks
Polymeric organic frameworks (POFs) are tunable and robust porous materials with potential applications for gas capture, catalysis, and separations technologies. A series of new porous POFs have been synthesized from the reaction of phloroglucinol or resorcinol derivatives with aryl aldehyde precursors. The monomers have various molecular shapes including linear, bent, trigonal, and tetrahedral geometries. Depending on the size and geometric matching of the monomers, the polymers are dominantly microporous with some mesoporous character or they are non-porous. In addition to standard spectroscopic and surface characterization, the materials were screened as adsorbents for carbon dioxide capture at low pressure (0-1 bar). The best performing material (POF 1D) has a CO 2 capture capacity of 9.0 wt. % (2.04 mmol g -1 ) at 298 K and 1 bar which is comparable to other polymeric organic frameworks. Isosteric heats of adsorption for POF 1A, POF 2A, and POF 2B were found to be dependent on the weight percent of CO 2 adsorbed: this suggests there are both chemisorptive and physisorptive components of CO 2 capture by the POFs.
RFQ-Structure Power Requirements: Analysis of Two Structure Designs
Abstract not provided.
Structural Design and Analysis of a Segmented Ultralight Morphing Rotor (SUMR) for Extreme-Scale Wind Turbines
Abstract not provided
Mariner Mars 1964 antenna structure design and development
Mariner Mars 1964 antenna design and development
Some basic guidelines for establishing structural design parameters for the landing gear of stable, soft landing spacecraft.
Soft landing spacecraft landing gear design for legged assemblies, discussing load, clearance and stability requirements