Results 11 to 20 of about 6,551 (166)

Study of Vortex Breakdown and Pitch up on a Compound Delta Wing [PDF]

open access: yesINCAS Bulletin, 2019
This paper discusses the calculation of mean pressure on a compound delta wing configuration and its variance to understand vortex breakdown and pitch up on the setup. The configuration of the compound delta wing being used was 50°-60°. The data was used
SHIVAM, Shashi Bhushan VERMA
doaj   +1 more source

Engineering Application of an Identification Method to Shock-Induced Vortex Stability in the Transonic Axial Fan Rotor

open access: yesInternational Journal of Aerospace Engineering, 2021
In the present paper, the steady RANS (Reynolds-Averaged Navier-Stokes) simulations based on our independently developed CFD (Computational Fluid Dynamics) solver NUAA-Turbo 2.0, are carried out to investigate the shock wave/tip leakage vortex (SW/TLV ...
Yan Xue, Ning Ge
doaj   +1 more source

Shock/Vortex Interaction and Vortex-Breakdown Modes [PDF]

open access: yes31st Aerospace Sciences Meeting, 1993
Computational simulation and study of shock/vortex interaction and vortex-breakdown modes are considered for bound (internal) and unbound (external) flow domains. The problem is formulated using the unsteady, compressible, full Navier-Stokes (NS) equations which are solved using an implicit, flux-difference splitting, finite-volume scheme.
O. A. Kandil, H. A. Kandil, C. H. Liu
openaire   +2 more sources

A coaxial vortex ring model for vortex breakdown [PDF]

open access: yesPhysica D: Nonlinear Phenomena, 2008
A simple - yet plausible - model for B-type vortex breakdown flows is postulated; one that is based on the immersion of a pair of slender coaxial vortex rings in a swirling flow of an ideal fluid rotating around the axis of symmetry of the rings. It is shown that this model exhibits in the advection of passive fluid particles (kinematics) just about ...
Blackmore, Denis   +2 more
openaire   +3 more sources

THE INFLUENCE OF FEATURES OF VORTEX FLOW ON AERODYNAMIC CHARACTERISTICS OF THE SUPERSONIC MANEUVERABLE AIRCRAFT MODEL

open access: yesНаучный вестник МГТУ ГА, 2019
The paper presents the influence of the vortex flow features, in particular, the phenomenon of vortex burst on the longitudinal and lateral aerodynamic characteristics of the maneuverable aircraft model with a sharp-edged fore-body.
K. A. Osipov
doaj   +1 more source

Very-Large-Eddy Simulation of Nonreactive Turbulent Flow for Annular Trapped Vortex Combustor [PDF]

open access: yesJournal of Applied Fluid Mechanics, 2022
A hybrid Reynolds-averaged Navier-Stokes (RANS) large eddy simulation (LES) method is applied in this work. It called very-large-eddy simulation (VLES) turbulence closure model.
K. Zhang, Y. Jin, X. Han, X. He
doaj   +1 more source

Vortex Breakdown in a Closed Cylindrical Container with a Rotating or Stationary Conical Endwall

open access: yesJournal of Fluid Science and Technology, 2010
A visualization study is made of flow of a constant-density viscous fluid in a closed cylindrical container. Fluid motions are generated by the rotation of one of its endwalls.
Kazuyuki FUJIMURA   +3 more
doaj   +1 more source

Mechanism of heat transportation in the intermediate wake of a heated cylinder

open access: yesNihon Kikai Gakkai ronbunshu, 2020
The paper clarifies the effects of buoyancy on the mechanism of heat transfer in the wake of heated cylinder for X/D=5-40. Measurements are made by a thermo-anemometer.
Hideaki WATANABE   +2 more
doaj   +1 more source

Anisotropic Characteristics of Turbulence Dissipation in Swirling Flow: A Direct Numerical Simulation Study

open access: yesAdvances in Mathematical Physics, 2015
This study investigates the anisotropic characteristics of turbulent energy dissipation rate in a rotating jet flow via direct numerical simulation. The turbulent energy dissipation tensor, including its eigenvalues in the swirling flows with different ...
Xingtuan Yang   +5 more
doaj   +1 more source

Flow Behavior in Side-View Plane of Pitching Delta Wing [PDF]

open access: yesEPJ Web of Conferences, 2018
In the present investigation, a delta wing which has 70° sweep angle, Λ was oscillated on its midcord according to the equation of α(t)=αm+α0sin(ωet). This study focused on understanding the effect of pitching and characterizing the interaction of vortex
Pektas Mehmet Can   +4 more
doaj   +2 more sources

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