High-fidelity flight maneuver simulations are crucial for the development of realistic digital aircraft models. However, such simulations are still hampered by difficulties in modeling the relative body motion between control and lifting surfaces when using realistic configurations. The presence of spanwise gaps between lifting and control surfaces impedes the application of concepts such as mesh deformation, and hampers the usage of mesh deformation combined with the overset method since the mesh generation process is particularly cumbersome. To reduce the user effort to create overset meshes, we have developed a methodology to automatically create overlapping regions for matching block interfaces. Hence, the usage of the overset method co...
With the recent focus on the needs of design and applications CFD, research groups have begun to add...
In this paper, mesh deformation based on radial basis function (RBF) interpolation is applied to the...
In this paper the problem of integrated design and control for a civil blended wing-body aircraft is...
High-fidelity flight maneuver simulations are crucial for the development of realistic digital aircr...
High-fidelity flight maneuver simulations are crucial for the development of realistic digital aircr...
High-fidelity flight maneuver simulations are crucial for the development of realistic digital aircr...
A deformable overset grid method is proposed to simulate the unsteady aerodynamic problems with mult...
This paper documents the initial development results of an efficient mesh deformation technique to s...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/143082/1/6.2017-3327.pd
In this paper, mesh deformation based on radial basis functions is employed for deflecting aircraft ...
This document describes different strategies to model 2D movable control surfaces. The system to be ...
Misc - august 2012.The presence of moving meshes when motions of fluids and solids are being simulat...
In this work, moving mesh methods based on the solution of pseudo structural and fluid problems are ...
During this workshop modelling and simulation techniques and related investigations over the past ye...
Advances in computational power allow the increase in the fidelity level of analysis tools used in c...
With the recent focus on the needs of design and applications CFD, research groups have begun to add...
In this paper, mesh deformation based on radial basis function (RBF) interpolation is applied to the...
In this paper the problem of integrated design and control for a civil blended wing-body aircraft is...
High-fidelity flight maneuver simulations are crucial for the development of realistic digital aircr...
High-fidelity flight maneuver simulations are crucial for the development of realistic digital aircr...
High-fidelity flight maneuver simulations are crucial for the development of realistic digital aircr...
A deformable overset grid method is proposed to simulate the unsteady aerodynamic problems with mult...
This paper documents the initial development results of an efficient mesh deformation technique to s...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/143082/1/6.2017-3327.pd
In this paper, mesh deformation based on radial basis functions is employed for deflecting aircraft ...
This document describes different strategies to model 2D movable control surfaces. The system to be ...
Misc - august 2012.The presence of moving meshes when motions of fluids and solids are being simulat...
In this work, moving mesh methods based on the solution of pseudo structural and fluid problems are ...
During this workshop modelling and simulation techniques and related investigations over the past ye...
Advances in computational power allow the increase in the fidelity level of analysis tools used in c...
With the recent focus on the needs of design and applications CFD, research groups have begun to add...
In this paper, mesh deformation based on radial basis function (RBF) interpolation is applied to the...
In this paper the problem of integrated design and control for a civil blended wing-body aircraft is...