Add to ORKGThis study focuses on three-dimensional evolution of unperturbed and perturbed leading-edge vortices over delta wings. Since the vortex filament method can discretize the high vorticity-containing region of vorticity fields and track this discretization in a Lagrangian frame, it is chosen to simulate the core of the leading-edge vortices. The purpose of perturbing the vortex core is to delay or suppress vortex breakdown over delta wings.Master of Engineering (MAE
It has been demonstrated that leading edge vortices (LEVs) formed by airflow past an elevated delta ...
In this paper, the reactive flow control of delta wing leading edge vortices using along-core pulse ...
117 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 1988.Vortex aerodynamics has playe...
This study focuses on three-dimensional evolution of unperturbed and perturbed leading-edge vortices...
A Computational method is presented for the calculation of the incompressible flow about wings with ...
SEE A90-458458th AIAA Applied Aerodynamics Conference; Aug. 20-22, 1990; Portland, OR; United States...
The overall goal of the research presented in this thesis is to extend the physical understanding of...
This thesis deals with Computational Fluid Dynamics (CFD)simulations of the flow around delta wings ...
A delta wing is subjected to small-amplitude perturbations over a range of periods, to simulate lead...
Computational aerodynamic studies were conducted to investigate the centerbody effects on the aerody...
Two artificial dissipation models, the original model of Jameson, Schmidt and Turkel. and its modifi...
A numerical simulation of vortex breakdown on a delta wing is carried out. Flow-field within and aro...
The present paper analyzes the vortical flow downstream of a delta wing. The Delta wing is designed ...
The dye injection and hydrogen bubble visualization techniques are used to investigate the dual-vort...
An experimental investigation on vortex breakdown on delta wings at high angles of attack is present...
It has been demonstrated that leading edge vortices (LEVs) formed by airflow past an elevated delta ...
In this paper, the reactive flow control of delta wing leading edge vortices using along-core pulse ...
117 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 1988.Vortex aerodynamics has playe...
This study focuses on three-dimensional evolution of unperturbed and perturbed leading-edge vortices...
A Computational method is presented for the calculation of the incompressible flow about wings with ...
SEE A90-458458th AIAA Applied Aerodynamics Conference; Aug. 20-22, 1990; Portland, OR; United States...
The overall goal of the research presented in this thesis is to extend the physical understanding of...
This thesis deals with Computational Fluid Dynamics (CFD)simulations of the flow around delta wings ...
A delta wing is subjected to small-amplitude perturbations over a range of periods, to simulate lead...
Computational aerodynamic studies were conducted to investigate the centerbody effects on the aerody...
Two artificial dissipation models, the original model of Jameson, Schmidt and Turkel. and its modifi...
A numerical simulation of vortex breakdown on a delta wing is carried out. Flow-field within and aro...
The present paper analyzes the vortical flow downstream of a delta wing. The Delta wing is designed ...
The dye injection and hydrogen bubble visualization techniques are used to investigate the dual-vort...
An experimental investigation on vortex breakdown on delta wings at high angles of attack is present...
It has been demonstrated that leading edge vortices (LEVs) formed by airflow past an elevated delta ...
In this paper, the reactive flow control of delta wing leading edge vortices using along-core pulse ...
117 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 1988.Vortex aerodynamics has playe...