The developed model is suitable for adoption for the design of a multi-product resilient Food Supply Chain that makes use of a multiple sourcing policy to deal with unexpected fluctuations of market demand and disruptions in raw materials supply.
This work helps alloy designers to determine the required chemical composition of a new alloy with reference to the temperature of application of that alloy and see the effect of temperature and composition on stable phases and associated properties of alloys.
In the present paper, a jet ejection cooling cycle is coupled to a 1.5 l diesel engine in order to cool down engine intake air by using waste heat recovery from engine exhaust gasses.
The difference in the supersonic aerodynamic characteristic of different wing planforms is evaluated to determine the optimum parameters for the cross-sectional geometry of a supersonic wing. Through design optimizations, the contributions of different cross-sectional parameters to drag...
This study applied Building Performance Optimization to the design of a newly built complex building. A number of design variables, including the shape of the building’s eaves, were optimized to improve building energy efficiency and indoor thermal comfort.
COMPOSELECTOR is an ambitious, innovative and timely project whose aim is to develop, demonstrate and assess an integrated software platform based on a multi-disciplinary, multi-model and multi-field approach for decision-making in the selection, design and fabrication of micro-...
The UTOPIAE project envisions the creation of a training and research network funded by the European Commission through the Horizon 2020 Programme, with the objective to train 15 Early Stage Researchers (ESRs) in the field of Uncertainty Quantification (UQ) and Optimization, providing...
The presentation emphasizes how the Air Force Research Laboratory delivers vehicles that satisfy mission requirements in a timely manner and reduce the number of late defects due to unmodeled physics.
BAE Systems OSI uses modeFRONTIER to determine the optimal configuration of propellant sticks that go into a motor in order to maximize the total number of build quantities and minimize overall performance risk across those motor builds.
