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2: Airbus A380 Fuel Tank Arrangement [113]

2: Airbus A380 Fuel Tank Arrangement [113]

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Figure 2.2: Example of a Design Structure Matrix (DSM)
Figure 2.3: Design Structure Matrix representation of the three...
Figure 2.4: Example of a House of Quality for a simplified aircraft...
Figure 2.5: Example of a morphological matrix
+37 Figure 2.9: Pareto graph for a 2-objective optimisation (minimisation)...
Set-Based Design and Optimisation of Aircraft Systems
Thesis
Full-text available
  • Apr 2018
During the early stages of any system design, a thorough exploration of the design space can prove to be challenging and computationally expensive. The challenges are further exacerbated when dealing with complex systems, such as an aircraft, due to the high dimensionality of their design space. Arising from the Toyota Product Development System, S...
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Table 1 . Aircraft level design parameters
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During the early stages of any system design, a thorough exploration of the design space can prove to be challenging and computationally expensive. The challenges are further exacerbated when dealing with complex systems, such as an aircraft, due to the high dimensionality of their design space. Arising from the Toyota Product Development System, s...
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Citations

... In the event of an APU pump failure, the wing tank pumps can be activated to supply fuel. The system's design minimizes the risk of operational disruptions due to mechanical issues [13]. Figure1, illustrate schematic fuel tank of A380. ...
A Simulation Study on Utilizing in Airbus380 fuel Tanks for Thrust and Fuel Efficiency
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  • May 2024
Citation: Anahita Moghtadaei (2024). A Simulation Study on Utilizing in Airbus380 fuel Tanks for Thrust and Fuel Efficiency. Eng OA, 2(2), 01-08. Abstract This paper explores the potential benefits of using nanofluids within the fuel system of an Airbus A380 to enhance engine thrust and reduce fuel consumption. By analyzing the Nusselt and Reynolds numbers, the study aims to understand the heat transfer and fluid dynamics that could lead to more efficient aircraft operation. The integration of nanotechnology in aviation fuel systems represents a promising frontier for improving aircraft performance. the nanoscale as a fluid whose particles are suspended between 1-100 nanometers and permanently in the particle. Adding nanoscale increases heat transfer. In this research used silicon carbide nanofluid (sic nanofluid) with a percentage of (1,2,3,4%) the base fluid (Jet A1) as well as thermal properties including Nusselt number and thermal conductivity coefficient and... It's been studied. Engineering: Open Access
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