Modelling and Design Optimization of a Novel Wide-Body Transport Aircraft to Improve the Structural Integrity

<table class="table-group" id="tab7"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Technologies</td><td class="align_center">Assumptions</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Advanced material and structures used</td><td class="align_center">20% structural weight reduction</td></tr><tr><td class="align_left">Boundary layer ingestion (BLI)</td><td class="align_center">40% of the <i>L</i><sub><i>f</i></sub> from the rear tail section</td></tr><tr><td class="align_left" rowspan="2">Upgraded efficient engine</td><td class="align_center">9.39 BPR with engine overall pressure ratio (OPR) 35 (ref: <a href="https://www.easa.europa.eu/en/downloads/7641/en" target="_blank">https://www.easa.europa.eu/en/downloads/7641/en</a>)</td></tr><tr><td class="align_center">High bypass ratio turbofan with TAPS</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Consideration of advanced technologies.</div>

Mathematical Problems in Engineering

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Table 7

Table 7: Modelling and Design Optimization of a Novel Wide-Body Transport Aircraft to Improve the Structural Integrity 