Abstract
This paper attempts to calculate the volume and surface area of an Airbus A350-900 aircraft using integration, and to optimise the dimensions of the aircraft while minimising the aerodynamic drag using Lagrange multipliers.
Information
This paper was submitted as the Internal Assessment for the May 2022 International Baccalaureate Mathematics Analysis and Approaches Higher Level exams.
Marks achieved: 16/20
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Paper License: CC BY-NC-SA 4.0