Large eddy simulation of micro vortex generator-controlled cavitation across multiple stages

C Mou, B Che, Y Wang, J Zhang, L Cao, D Wu - Physics of Fluids, 2024 - pubs.aip.org
Micro vortex generators (mVGs) control cavitation by altering the boundary layer flow
structure. This study employs the wall-adapting local eddy-viscosity large eddy simulation …

Turbulence modeling approaches on unsteady flow structures around a semi-circular cylinder

S Yagmur, S Dogan, MH Aksoy, I Goktepeli - Ocean Engineering, 2020 - Elsevier
This paper presents the flow field around a Semi-Circular Cylinder (SCC), a basic geometry
for fluid mechanics, obtained numerically by Computational Fluid Dynamics (CFD) at …

Flow and thermal characteristics of jet impingement on a flat plate for small nozzle to plate spacing using LES

AK Shukla, A Dewan - International Journal of Thermal Sciences, 2019 - Elsevier
This paper presents a study of flow and thermal characteristics of jet impingement heat
transfer by large eddy simulation (LES) using the wall adapting local eddy (WALE) viscosity …

Effect of von Karman length scale in scale adaptive simulation approach on the prediction of supersonic turbulent flow

CY Xu, T Zhang, YY Yu, JH Sun - Aerospace Science and Technology, 2019 - Elsevier
Numerical investigations of the supersonic axisymmetric base flow at Mach number 2.46
and Reynolds number 2.858× 10 6 are carried out using the scale-adaptive simulation …

Flow-dependent DDES/γ− Re‾ θt coupling model for the simulation of separated transitional flow

L Zhou, Z Gao, Y Du - Aerospace Science and Technology, 2019 - Elsevier
A new DDES and γ− R e‾ θ t coupling model for separated transitional flow is proposed. The
studies in this paper indicate that the activation of the LES branch in the free stream may …

Unsteady Detached-Eddy Simulation (DES) of the Jetstream 31 aircraft in One Engine Inoperative (OEI) condition with propeller modelling

L Casadei, L Könözsy, NJ Lawson - Aerospace Science and Technology, 2019 - Elsevier
Numerical results from a three-dimensional (3D) computational fluid dynamics (CFD) model
of the Jetstream 31 aircraft in conditions of one engine inoperative are presented. The …

Numerical simulation for the decomposition of DT-3 in a monopropellant thruster

Z Gao, G Li, T Zhang, X Liu, Z Wang, X Liu - Aerospace Science and …, 2018 - Elsevier
DT-3 is a high performance low-freezing monopropellant developed in the 1980s in China,
DT-3 is also the world's first practical use of low freezing point propellant. As a …

Inward turning base-bleed technique for base drag reduction

S Paul, AV Raj, CS Kumar - The Aeronautical Journal, 2023 - cambridge.org
This paper consists of CFD and experimental study for shell projectile at angle of attack 00
and at various Mach numbers (0.7, 0.9, 1.0, 1.5 and 2.0), without spin effect. Passive method …

Optimization of artillery projectiles base drag reduction using hot base flow

MA Dali, S Jaramaz - Thermal Science, 2019 - doiserbia.nb.rs
The CFD numerical simulations were carried out to investigate the base drag characteristics
of a projectile with base bleed unit with a central jet. Different base bleed grain types with …

CFD study of self-cleaning system of multi-stage tangential roller threshing unit for precise buckwheat breeding

S Hussain, H Jianjun, C Yong, A Ali, H Song, D Zheng… - Heliyon, 2024 - cell.com
Buckwheat is a globally recognized, nutritionally rich crop with robust adaptability, serving
as a multi-purpose plant for its health benefits. Achieving precise and mechanized plot seed …