In the previous project, you explained the thermodynamic developments. What are the differences in thrust, fuel consumption, and emissions?
What are the differences in thrust fuel consumption and emissions?
In the previous project, you explained the thermodynamic developments.
Here you will address the design changes to maximize the thermodynamics.
Commercial aircraft engines have evolved and been developed to improve reliability, reduce fuel consumption, and lower emissions.
Select from the aircraft list below and research the engines used when first launched and those used now.
A320
B737
B747
A330
B52
B777
First, what are the differences in thrust, fuel consumption, and emissions?
Secondly, discuss the thermodynamic design improvements that have occurred and review in a systems description.
Also, What has changed in the design of these newer versions of jet engines?
More Details;
First, various aspects of a multi-disciplinary aero engine conceptual design approach and computational framework are presented.
Secondly, the approach closely integrates different disciplines and is capable of homing in on the best designs in the presence of techno-economic and environmental risk.
Consequently, the framework can assist in the transition from the traditional, human-centered design procedure that involves complex manual iterations, to a more automated process.
It considers the following disciplines: engine performance, engine aerodynamic and mechanical design, aircraft design and aerodynamic performance, emissions prediction and environmental impact, engine and airframe noise, and production, maintenance and direct operating costs.
In addition, the proposed explicit conceptual design algorithm reduces system complexity, improves computational speed and can make design space exploration and optimization results easier to interpret.
More so, these range from technology assessment and design sensitivity analysis to design space exploration and optimization.
Overall, the work sets the necessary base for an assessment methodology that can quantify risks and assess the impact of gas turbine design on the environment, by comparing and helping to rank future technologies and design concepts for civil aviation on a formal and consistent basis.
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