Graphene‐Based Pressure Sensor Application in Non‐Invasive Pulse Wave Velocity Continuous Estimation
A non‐invasive device prototype for pulse wave velocity (PWV) measurement is presented, based on a piezoelectric graphene pressure sensor incorporating advanced electronic components and data analysis tools. Tests performed within clinical environment, showed statistical similarity to results obtained using the established standard for PWV estimation ...
Irene Buraioli+9 more
wiley +1 more source
Stabilization of Hypersonic Boundary Layers by Porous Coatings [PDF]
A second-mode stability analysis has been performed for a hypersonic boundary layer on a wall covered by a porous coating with equally spaced cylindrical blind microholes.
Fedorov, Alexander V.+2 more
core +1 more source
A functionally graded oxide scale comprising a dense top layer and an underlying fine‐grained layer with a grain size gradient forms on a multicomponent (Hf,Zr,Ti)B2 coating through Ti content optimization. The former is a superior oxygen barrier, and the latter ensures strain tolerance, collectively manifesting the coating's exceptional ablation ...
Junshuai Lv+9 more
wiley +1 more source
The two extremes of self‐assembled colloids are stiff perfect crystals and soft perfect glasses. But what happens in between? The answer is provided by elasticity mapping of a wide variety of colloidal glasses – continuous gradient structures, binary mixtures, and more – with scanning micro‐Brillouin light scattering.
Thomas Vasileiadis+5 more
wiley +1 more source
Assessment of a high-order shock-capturing central-difference scheme for hypersonic turbulent flow simulations [PDF]
High-speed turbulent flows are encountered in most space-related applications (including exploration, tourism and defense fields) and represent a subject of growing interest in the last decades. A major challenge in performing high-fidelity simulations of such flows resides in the stringent requirements for the numerical schemes to be used.
arxiv
Rarefied hypersonic flow simulations using the Navier-Stokes equations with non-equilibrium boundary conditions [PDF]
This paper investigates the use of Navier-Stokes-Fourier equations with non-equilibrium boundary conditions (BCs) for simulation of rarefied hypersonic flows.
Greenshields, Christopher, Reese, Jason
core +1 more source
Bipolar HiPIMS kick‐pulse for high hardness in high‐entropy boride thin films
Abstract We report a microhardness indentation study for multicomponent refractory metal boride thin films that belong to the family of high‐entropy ceramics exhibiting superior hardness and high temperature properties. We focus on the nominally equimolar composition (Ti0.2Zr0.2Hf0.2Nb0.2Ta0.2)B2, which we refer to as HEB3, on c‐plane sapphire ...
Nathaniel S. McIlwaine+7 more
wiley +1 more source
Laminar boundary-layer separation and near-wake flow for a smooth blunt body at supersonic and hypersonic speeds. [PDF]
Jean-Marie Grange+2 more
openalex +2 more sources
Optimum maneuvers of hypervelocity vehicles [PDF]
Optimum maneuvering of glide vehicle at hypersonic ...
Busemann, A., Kelley, G. F., Vinh, N. X.
core +1 more source
Investigation of the double ramp in hypersonic flow using luminescent measurement systems [PDF]
Compression ramp flows in supersonic and hypersonic environments present unique flow patterns for shock wave-boundary layer interaction studies. They also represent the generic geometry of two-dimensional inlets and deflected control surfaces for re ...
Anderson+42 more
core +1 more source