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Conclusion Konstantinos G. Kyprianidis targets such as low weight and pressure losses for the intercooler and recuperator components. The commercial competitiveness of these designs will largely depend on how the aviation market evolves in the years to come until 2020. 8.2 Recommendations for future work Future work on the developed tool could focus on: • Consideration of engine deteriorated performance. Specific com- ponent technologies that aim to reduce engine performance deterioration could then be assessed more rigorously in terms of block fuel and direct operating costs. • More detailed consideration of an engine’s secondary air system. Large cooling and sealing flows could very well reduce, or even negate, the specific fuel consumption benefits predicted for some novel technologies and concepts. • An enhanced link between engine performance and WeiCo. This could assist in the transition from designing a turbine at a fixed point in the Smith chart to being able to trade turbine efficiency for stage count and weight during the optimisation process. • Introduction of transient performance aspects. For example a ground idle to take-off thrust acceleration could be considered, including thermal inertia effects for heat-exchanged cycles. • Further development of the HERMES code. The newly-added rou- tines for aircraft weight breakdown calculations formed the first step in the transformation of HERMES into a capable aircraft conceptual design tool. Consideration of center of gravity, fuselage design, wing buffet, and aircraft production costing aspects are the next steps to take. • Introduction of Air Traffic Management (ATM) and airline fleet operational aspects. Interesting and more realistic assessments could come out of such a development, including looking into ways of reducing an airline’s environmental footprint. 178PDF Image | Multi-disciplinary conceptual design of future jet engine systems
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