Add to ORKGRecent computational methods for more efficient and accurate quantification of unsteady aerodynamic loads on the aircraft
For an accurate prediction of the steady and unsteady behaviour of an aircraft it is necessary to ta...
In this thesis, the exploitation of computational fluid dynamics (CFD) methods for the flight dynami...
In the past decade, there has been much activity in the development of computational methods for the...
Each slight perturbation to a trimmed aircraft state causes additional aerodynamic loads on the airc...
Efficient and accurate prediction of derivatives from aerodynamic forces and moments of aircrafts ar...
The exploitation of computational fluid dynamics for non linear aeroelastic simulations is mainly ba...
Within the AVT-201 Task Group a comprehensive research program has been designed to assess the abili...
The paper presents the application of computational aeroelasticity (CA) methods to the analysis of a...
Determining the flutter boundaries for full aircraft configurations by time-accurately solving the R...
A systematic study is presented to guide the selection of a numerical solution strategy for URANS co...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90736/1/AIAA-2011-6525-438.pd
Computational aeroelasticity is vital to modern aircraft design, as common objectives and aeroelasti...
ABSTRACTOne key task in computational aeroelasticity is to calculate frequency response functions of...
This paper presents cross comparisons and assessments of the aerodynamic results obtained within the...
Calculating the flutter boundary by solving the Reynolds averaged Navier Stokes (RANS) equations in ...
For an accurate prediction of the steady and unsteady behaviour of an aircraft it is necessary to ta...
In this thesis, the exploitation of computational fluid dynamics (CFD) methods for the flight dynami...
In the past decade, there has been much activity in the development of computational methods for the...
Each slight perturbation to a trimmed aircraft state causes additional aerodynamic loads on the airc...
Efficient and accurate prediction of derivatives from aerodynamic forces and moments of aircrafts ar...
The exploitation of computational fluid dynamics for non linear aeroelastic simulations is mainly ba...
Within the AVT-201 Task Group a comprehensive research program has been designed to assess the abili...
The paper presents the application of computational aeroelasticity (CA) methods to the analysis of a...
Determining the flutter boundaries for full aircraft configurations by time-accurately solving the R...
A systematic study is presented to guide the selection of a numerical solution strategy for URANS co...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90736/1/AIAA-2011-6525-438.pd
Computational aeroelasticity is vital to modern aircraft design, as common objectives and aeroelasti...
ABSTRACTOne key task in computational aeroelasticity is to calculate frequency response functions of...
This paper presents cross comparisons and assessments of the aerodynamic results obtained within the...
Calculating the flutter boundary by solving the Reynolds averaged Navier Stokes (RANS) equations in ...
For an accurate prediction of the steady and unsteady behaviour of an aircraft it is necessary to ta...
In this thesis, the exploitation of computational fluid dynamics (CFD) methods for the flight dynami...
In the past decade, there has been much activity in the development of computational methods for the...