Add to ORKGA collaborative research on optimization of a main rotor blade for helicopters by JAXA, ONERA and DLR is underway. As a first step, blade optimization method with five design variables is explored by dealing with hovering conditions. Optimizations and simulations are carried out by each agency with their own analysis codes and these results are cross-validated. This paper presents an overview of the project and an interim report on the results obtained so far
Structural optimization of a helicopter rotor blade with uniform aerodynamic surface and twist at th...
This paper presents a survey of applications of design optimization to helicopter problems carried o...
Purpose - The purpose of this paper is to present the aerodynamic blade design of a tiltwing aircraf...
A cooperation on the aerodynamic optimization of helicopter rotors has been formed by JAXA, ONERA an...
A cooperation between JAXA, ONERA and DLR puts the focus on the aerodynamic optimization of helicopt...
The three research organizations, JAXA, ONERA and DLR have decided to combine their efforts in 2019 ...
The aerodynamic design of rotor blades is challenging, and is crucial for the development of helicop...
Onera and DLR are both national research centres involved in aeronautic research since early 1900. I...
The motivation of this work is to reduce the overall required computational resources of the aerodyn...
Industrial aerodynamic design optimization of helicopter rotor blades requires employ-ment of multi-...
Communication to : Twenty first European Rotorcraft Forum, Saint-Petersburg (Russia), August 30 - Se...
Described is a formal optimization procedure for helicopter rotor blade design which minimizes hover...
Within the DLR project VicToria an aerodynamic and aero-acoustic optimization of helicopter rotor bl...
This paper describes a joint activity involving NASA and Army researchers at the NASA Langley Resear...
Onera and DLR are both national research centres involved in aeronautic research since early 1900. I...
Structural optimization of a helicopter rotor blade with uniform aerodynamic surface and twist at th...
This paper presents a survey of applications of design optimization to helicopter problems carried o...
Purpose - The purpose of this paper is to present the aerodynamic blade design of a tiltwing aircraf...
A cooperation on the aerodynamic optimization of helicopter rotors has been formed by JAXA, ONERA an...
A cooperation between JAXA, ONERA and DLR puts the focus on the aerodynamic optimization of helicopt...
The three research organizations, JAXA, ONERA and DLR have decided to combine their efforts in 2019 ...
The aerodynamic design of rotor blades is challenging, and is crucial for the development of helicop...
Onera and DLR are both national research centres involved in aeronautic research since early 1900. I...
The motivation of this work is to reduce the overall required computational resources of the aerodyn...
Industrial aerodynamic design optimization of helicopter rotor blades requires employ-ment of multi-...
Communication to : Twenty first European Rotorcraft Forum, Saint-Petersburg (Russia), August 30 - Se...
Described is a formal optimization procedure for helicopter rotor blade design which minimizes hover...
Within the DLR project VicToria an aerodynamic and aero-acoustic optimization of helicopter rotor bl...
This paper describes a joint activity involving NASA and Army researchers at the NASA Langley Resear...
Onera and DLR are both national research centres involved in aeronautic research since early 1900. I...
Structural optimization of a helicopter rotor blade with uniform aerodynamic surface and twist at th...
This paper presents a survey of applications of design optimization to helicopter problems carried o...
Purpose - The purpose of this paper is to present the aerodynamic blade design of a tiltwing aircraf...