The unique demands of rotorcraft aeromechanics analysis have led to the development of software tools that are described as comprehensive analyses. The next generation of rotorcraft comprehensive analyses will be driven and enabled by the tremendous capabilities of high performance computing, particularly modular and scaleable software executed on multiple cores. Development of a comprehensive analysis based on high performance computing both demands and permits a new analysis architecture. This paper describes a vision of the requirements for this next generation of comprehensive analyses of rotorcraft. The requirements are described and substantiated for what must be included and justification provided for what should be excluded. With th...
The use of a computer program for a comprehensive analytical model of rotorcraft aerodynamics and dy...
This dissertation describes three aspects of the comprehensive rotorcraft analysis. First, a physics...
AbstractThis article presents a new mathematical model for helicopter comprehensive analysis with th...
AbstractThe history, status and lessons of a comprehensive analysis for rotorcraft are reviewed. The...
The development and application of comprehensive rotorcraft analysis methods in the field of rotorcr...
The history, status, and lessons of a comprehensive analysis for rotorcraft are reviewed. The develo...
Results from the comprehensive analysis CAMRAD II are presented, illustrating recent developments in...
Results from the comprehensive analysis CAMRAD II are presented, illustrating recent developments in...
Rapid advances in the technology of electronic digital computers and the need for an integrated synt...
An assessment of the status of helicopter theory and analysis is presented. The technology level emb...
Rotor dynamic analysis, which requires extensive amount of data and rigorous analytical processing, ...
A new comprehensive aeromechanics code for rotary wing aircraft is being developed at the German Aer...
In this paper, various small-sized modules are combined with one another in order to perform rotorcr...
The diversity of concept of rotorcrafts is only matched by their extent of application field. Then a...
Advanced rotorcraft configurations are being investigated with the objectives of identifying vehicle...
The use of a computer program for a comprehensive analytical model of rotorcraft aerodynamics and dy...
This dissertation describes three aspects of the comprehensive rotorcraft analysis. First, a physics...
AbstractThis article presents a new mathematical model for helicopter comprehensive analysis with th...
AbstractThe history, status and lessons of a comprehensive analysis for rotorcraft are reviewed. The...
The development and application of comprehensive rotorcraft analysis methods in the field of rotorcr...
The history, status, and lessons of a comprehensive analysis for rotorcraft are reviewed. The develo...
Results from the comprehensive analysis CAMRAD II are presented, illustrating recent developments in...
Results from the comprehensive analysis CAMRAD II are presented, illustrating recent developments in...
Rapid advances in the technology of electronic digital computers and the need for an integrated synt...
An assessment of the status of helicopter theory and analysis is presented. The technology level emb...
Rotor dynamic analysis, which requires extensive amount of data and rigorous analytical processing, ...
A new comprehensive aeromechanics code for rotary wing aircraft is being developed at the German Aer...
In this paper, various small-sized modules are combined with one another in order to perform rotorcr...
The diversity of concept of rotorcrafts is only matched by their extent of application field. Then a...
Advanced rotorcraft configurations are being investigated with the objectives of identifying vehicle...
The use of a computer program for a comprehensive analytical model of rotorcraft aerodynamics and dy...
This dissertation describes three aspects of the comprehensive rotorcraft analysis. First, a physics...
AbstractThis article presents a new mathematical model for helicopter comprehensive analysis with th...