Saeed HOSSEINI, Mohammad Ali VAZIRY-ZANJANY

DOI Number: 10.82241ceas-hisst-2024-292

Conference number: HiSST-2024-292

An aircraft design framework is developed and employed for the optimization of a Mach 1.6, 7000 km range, 72-passenger aircraft, to minimize aircraft weight, cost, emission, and noise. To this aim, the aircraft configuration is designed, and a base layout is developed using rapid engineering methods and area ruling requirements. This base layout is then optimized in the developed framework concerning weight, cost, emission, and noise objectives. The core disciplines of the optimization framework are Requirements, Weight, Sizing, Geometry, Aerodynamics, Engine, Performance, Cost, Emission, Noise, and Optimization. High-fidelity CAD and FEA processes are used to loft the aircraft’s external surface and estimate the wing weight, respectively.

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In Categories: 1.Events, High-Speed Missions and Vehicles, HiSST 2024
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