Thesis (Ph.D.)--University of Washington, 2019The application of an integrated model based process to the design of the structure of an engine pylon at a level of detail and thoroughness that would meet certification requirements leads to significant time and cost savings as well as resulting structure with high strength to weight ratio. Numerous technological hurdles to rapidly generate design synthesis pylon models have been cleared. Newly created modular automation platform (MAP) paves the path, implementing the multi-level sizing process, to model based design synthesis process for pylon certification driven by gradient based optimization algorithm. The integrated model based process introduced in this work can be further extended to th...
Modern 3D CAD permanently modifies the development process of most industrial products. The traditio...
In this paper, a knowledge-based approach to support analysis model generation is proposed, which ai...
The Flying-V is an unconventional aircraft concept showing promising initial results in overall effi...
The aircraft design process is a complex, highly iterative, time-consuming process that contributes ...
Designing an airframe is a complex process as it requires knowledge from multiple disciplines such a...
International audienceIn the context of fuel consumption reduction, integrated power-plant system op...
Aircraft engine technology has evolved and matured over a 70 year period under a continous pressure ...
The aircraft design process can generally be classified into three major phases. In the conceptual d...
The state-of-the-art methods in preliminary wing design are using models employing physics-based met...
The product development cycles in all parts of the industry become increasingly shorter. In spite of...
A procedure is developed for the optimum sizing of wing structures based on representing the built-u...
Engineering design may be viewed as a decision making process that supports design tradeoffs. The de...
Aircraft structural layout concept design at Saab Aeronautics utilize thickness optimizationto evalu...
The current structural sizing process used to design military aircraft was developed when the emphas...
Turbo machinery preliminary design is an iterative process that begins with an initial Cycle design ...
Modern 3D CAD permanently modifies the development process of most industrial products. The traditio...
In this paper, a knowledge-based approach to support analysis model generation is proposed, which ai...
The Flying-V is an unconventional aircraft concept showing promising initial results in overall effi...
The aircraft design process is a complex, highly iterative, time-consuming process that contributes ...
Designing an airframe is a complex process as it requires knowledge from multiple disciplines such a...
International audienceIn the context of fuel consumption reduction, integrated power-plant system op...
Aircraft engine technology has evolved and matured over a 70 year period under a continous pressure ...
The aircraft design process can generally be classified into three major phases. In the conceptual d...
The state-of-the-art methods in preliminary wing design are using models employing physics-based met...
The product development cycles in all parts of the industry become increasingly shorter. In spite of...
A procedure is developed for the optimum sizing of wing structures based on representing the built-u...
Engineering design may be viewed as a decision making process that supports design tradeoffs. The de...
Aircraft structural layout concept design at Saab Aeronautics utilize thickness optimizationto evalu...
The current structural sizing process used to design military aircraft was developed when the emphas...
Turbo machinery preliminary design is an iterative process that begins with an initial Cycle design ...
Modern 3D CAD permanently modifies the development process of most industrial products. The traditio...
In this paper, a knowledge-based approach to support analysis model generation is proposed, which ai...
The Flying-V is an unconventional aircraft concept showing promising initial results in overall effi...