Results 21 to 30 of about 9,245 (265)

Characterization of Supersonic Compressible Fluid Flow Using High-Speed Interferometry

open access: yesSensors, 2021
This paper presents a very effective interference technique for the sensing and researching of compressible fluid flow in a wind tunnel facility. The developed technique is very sensitive and accurate, yet easy to use under conditions typical for ...
Pavel Psota   +10 more
doaj   +1 more source

Supersonic Ejector with a Tangential Supersonic Nozzle

open access: yesNTU "KhPI" Bulletin: Power and heat engineering processes and equipment
The flow rate and impulse characteristics of supersonic ejectors, where supersonic and subsonic streams typically interact, are determined not only by the interaction area between the supersonic jet and the entrained flow, but also by the pressure field in the ejector mixing chamber.
Gennadii Voropaiev, Nazariy Kolodii
openaire   +3 more sources

Screen-Printed PVDF Piezoelectric Pressure Transducer for Unsteadiness Study of Oblique Shock Wave Boundary Layer Interaction

open access: yesMicromachines
Shock wave boundary/layer interactions (SWBLIs) are critical in high-speed aerodynamic flows, particularly within supersonic regimes, where unsteady dynamics can induce structural fatigue and degrade vehicle performance.
Bei Wang   +8 more
doaj   +1 more source

Effect of Quasi-Static Door Operation on Shear Layer Bifurcations in Supersonic Cavities

open access: yesAerospace
Span-wise homogeneous supersonic cavity flows display complicated structures due to shear layer breakdown, flow acoustic resonance, and even non-linear hydrodynamic-acoustic interactions. In practical applications, such as aircraft bays, the cavity is of
Skyler Baugher   +5 more
doaj   +1 more source

Study on Flow Characteristic of Sub-/Super-Sonic Mixing Layer

open access: yesXibei Gongye Daxue Xuebao, 2020
In order to obtain the flow characteristics of sub-super-sonic mixing layer including velocity distribution, pressure distribution and development of mixing layer, experimental and numerical investigations were conducted.

doaj   +1 more source

A Unified Asymptotic Theory of Supersonic, Transonic, and Hypersonic Far Fields

open access: yesAxioms, 2022
The problems of steady, inviscid, isentropic, irrotational supersonic plane flow passing a body with a small thickness ratio was solved by the linearized theory, which is a first approximation at and near the surface but fails at far fields from the body.
Lung-Jieh Yang, Chao-Kang Feng
doaj   +1 more source

Computational Fluid Dynamics and Adjoint-Based Optimization of a Supersonic Combustor for Improved Efficiency

open access: yesFluids
Adjoint-based optimization methods, that were previously in the realm of computational fluid dynamics (CFD) research, are now available in commercial software.
Carola Rovira Sala   +3 more
doaj   +1 more source

Implicit Subgrid-Scale Modeling of a Mach 2.5 Spatially Developing Turbulent Boundary Layer

open access: yesEntropy, 2022
We employ numerically implicit subgrid-scale modeling provided by the well-known streamlined upwind/Petrov–Galerkin stabilization for the finite element discretization of advection–diffusion problems in a Large Eddy Simulation (LES) approach. Whereas its
Guillermo Araya, Christian Lagares
doaj   +1 more source

European Standard Clinical Practice Guideline and EXPeRT Recommendations for the Diagnosis and Management of Gastroenteropancreatic Neuroendocrine Neoplasms in Children and Adolescents

open access: yesPediatric Blood &Cancer, EarlyView.
ABSTRACT Pediatric gastroenteropancreatic neuroendocrine neoplasms (GEP‐NENs) are extremely rare and clinically heterogeneous. Management has largely been extrapolated from adult practice. This European Standard Clinical Practice Guideline (ESCP), developed by the EXPeRT network in collaboration with adult NEN experts, provides (adult) evidence ...
Michaela Kuhlen   +23 more
wiley   +1 more source

Interaction of the Shock Train Leading Edge and Filamentary Plasma in a Supersonic Duct

open access: yesFluids
Quasi-direct current (Q-DC) filamentary electrical discharges are used to control the shock train in a back-pressured Mach 2 duct flow. The coupled interaction between the plasma filaments and the shock train leading edge (STLE) is studied for a variety ...
Loren C. Hahn   +3 more
doaj   +1 more source

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