Experimental verification of an analytical determination of overall thermal conductivity of honeycomb-core panels
Analytical determination of thermoconductivity of honeycomb-core panels fabricated from cobalt-base alloy
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Analytical determination of thermoconductivity of honeycomb-core panels fabricated from cobalt-base alloy
Ultralight honeycomb development for Saturn S-II STAGE improvement - titanium bonding, core sandwich construction, and testing
Energy dissipating plastic honeycomb
Energy dissipating plastic honeycomb materials
Design of heavy-gauge bonded honeycomb sandwich
Visual observation inspection device for bonded honeycomb sandwich structures using birefringent plastic coatings
Nondestructive testing techniques for Saturn honeycomb heat shields
Phenolic honeycomb as energy dissipator
Developmental testing of energy dissipating plastic honeycomb
Manufacturing modifications, and glass filler additions for dip resin used in honeycomb structures
Development of nondestructive testing system, using ultrasonic techniques, for detecting disbonds in composite honeycomb heat shields of Saturn launch vehicle
Literature and industrial surveys of nondestructive testing equipment and techniques for application to honeycomb heat shields, including partially annotated bibliography
Brazing alloy development for high strength aluminum honeycomb sandwich composites for elevated and cryogenic temperature applications
Energy dissipating plastic dovetail honeycomb
Fabrication and testing of dovetail plastic honeycomb structures for landing shock absorbers
Ultrasonic techniques for nondestructive testing for Saturn honeycomb heat shields
This work explains that the properties of Al 5052 material used commonly for honeycomb cores in sandwich panels are highly dependent on the tempering condition. It has not been common to specify the temper when ordering HC material nor is it common for the supplier to state what the temper is. For aerospace uses, a temper of H38 or H39 is probably recommended. This temper should be stated in the bill of material and should be verified upon receipt of the core. To this end some properties provided herein can aid as benchmark values.
Quantum simulations of many-body systems are among the most promising applications of quantum computers. In particular, models based on strongly correlated fermions are central to our understanding of quantum chemistry and materials problems, and can lead to exotic, topological phases of matter. However, owing to the non-local nature of fermions, such models are challenging to simulate with qubit devices. Here we realize a digital quantum simulation architecture for two-dimensional fermionic systems based on reconfigurable atom arrays. We utilize a fermion-to-qubit mapping based on Kitaev’s model on a honeycomb lattice, in which fermionic statistics are encoded using long-range entangled states. We prepare these states efficiently using measurement and feedforward, realize subsequent fermionic evolution through Floquet engineering with tunable entangling gates interspersed with atom rearrangement, and improve results with built-in error detection. Leveraging this fermion description of the Kitaev spin model, we efficiently prepare topological states across its complex phase diagram and verify the non-Abelian spin-liquid phase by evaluating an odd Chern number. We further explore this two-dimensional fermion system by realizing tunable dynamics and directly probing fermion exchange statistics. Finally, we simulate strong interactions and study the dynamics of the Fermi–Hubbard model on a square lattice. These results pave the way for digital quantum simulations of complex fermionic systems for materials science, chemistry and high-energy physics.