The propulsion system consists of two , each with a thrust rating of 40,000 pounds. The engines are mounted under the wing, with a pylon and engine mount system.
The objective of the Aircraft Design Project 2 is to design a commercial aircraft that meets specific requirements and constraints. The project is divided into several phases, including conceptual design, preliminary design, and detailed design. The goal is to create a safe, efficient, and economically viable aircraft that can be used for short-haul flights. aircraft design project 2 report pdf
Aircraft Design Project 2 Report PDF**