We show that density-weighted moments of the dissipation rate, epsilonl, averaged over a scale l, in supersonic turbulence can be successfully explained by the She and Lévêque model [Phys. Rev. Lett. 72, 336 (1994)]. A general method is developed to measure the two parameters of the model, gamma and d, based directly on their physical interpretations as the scaling exponent of the dissipation rate in the most intermittent structures (gamma) and the dimension of the structures (d). We find that the best-fit parameters (gamma=0.71 and d=1.90) derived from the epsilonl scalings in a simulation of supersonic turbulence at Mach 6 agree with their direct measurements, confirming the validity of the model in supersonic turbulence.
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http://dx.doi.org/10.1103/PhysRevLett.102.034501 | DOI Listing |
ACS Omega
November 2024
College of Mechanical and Electronic Engineering, Shandong University of Science and Technology, Qingdao 266590, China.
To improve the dry powder jet extinguishing efficiency, the velocity change and spatial distribution of ultrafine dry powder particles under the action of high Mach number compressible air are studied by using the SST turbulence model and the gas-solid two-phase coupled model. The effects of nozzle pressure ratio, particle diameter, and mass flow on parameters such as Mach number and radial diffusion width are analyzed,and the influence of injection pressure and jet performance is verified by ultrafine dry powder jet experiment. The results show that the increase in the particle size will weaken particle flowability; the Saffman lift force has a significant effect on the particles when the nozzle expansion angle is large, and a particle-free zone is produced near the center axis; increasing the nozzle pressure ratio or reducing the dry powder mass flow rate will help improve the particle velocity in the core jet area outside the nozzle, and the accuracy of this law is proved by experiments.
View Article and Find Full Text PDFWhen a hypersonic seeker flies at high speed within the atmosphere, intense interaction with the incoming flow gradually develops into a complex turbulent flow field. This interaction results in complex thermal responses at the seeker window, causing aerodynamic optical effects such as image shift, jitter, and blur of the target image, thereby restricting the seeker's detection capability and accuracy. This paper uses a numerical simulation model for the guidance performance of a hypersonic seeker under aerodynamic optical transmission effects.
View Article and Find Full Text PDFSci Adv
November 2024
Universität Hamburg, Hamburger Sternwarte, Gojenbergsweg 112, 21029 Hamburg, Germany.
Supersonic turbulence occurs in many environments, particularly in astrophysics. In the crucial case of isothermal turbulence, the probability density function (PDF) of the logarithmic density, , is well measured, but a theoretical understanding of the processes leading to this distribution remains elusive. We investigate these processes using Lagrangian tracer particles to track and [Formula: see text] in direct numerical simulations, and we show that their evolution can be modeled as a stochastic differential process with time-correlated noise.
View Article and Find Full Text PDFJ Acoust Soc Am
September 2024
Institute of Fluid Science, Tohoku University, 2-1-1 Katahira, Aoba, Sendai, 980-8577, Japan.
ACS Omega
August 2024
Lab of Mechanical Structure & Biomechanics, Anhui Agricultural University, Hefei 230036, China.
As the core of a hypersonic propulsion system, the effective mixing efficiency of fuel and air in a supersonic combustor is crucial for its performance. This study focuses on a cold supersonic flow and employs computational fluid dynamics (CFD) techniques combined with Euler-Lagrange method's discrete-phase model (DPM) for multiphase flows, K-H and R-T (Kelvin-Helmholtz and Rayleigh-Taylor) mixing and atomization models, turbulence models, and surface evaporation models to investigate the injection, atomization, and mixing characteristics of kerosene in supersonic airflow. In order to enhance the mixing efficiency between kerosene and air while reducing flow losses, this study examines a staggered dual-jet injection scheme, with the dual jets arranged at the center of the cavity and having a dual-jet spacing of 10 and 20 mm, respectively.
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