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Optimization of fuels for the maximum thrust to drag ratio or specific impulse must consider the linkage of geometric restraints on the selection of fuel materials.
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While the researchers have made the significant effort on new technology & product design, optimized operations, and alternate fuels etc. for the optimization of fuel consumption in aviation industry, certain important issues remain unexplored.
Shape optimization of fuel channels in solid oxide fuel cells (SOFC) is presented.
Optimization of fuel consumption is a key driver in the design of spacecraft maneuvers.
The proposed approach allows for efficient and reliable multivariable optimization of fuel cell designs.
The model is useful for optimization of fuel cell design and operating conditions.
It involves the simultaneous optimization of fuel cost and emission objectives which are conflicting ones.
In the first step, optimization of fuel composition was implemented by cell calculations.
Mathematical models and simulation are needed as tools for design optimization of fuel cells, stacks and fuel cell power systems.
Different techniques for optimization of fuel loading pattern in the reactor core have been introduced by now.
Important industrial feedback results from operation and optimization of fuel cycle backend facilities, which is summarized in the paper.
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