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

Table 1

Component density factor of transport aircraft [10].

Component installation	Notation
Engine installed on the wing, fuel tank in the wing		0.003–0.0035
Transport, cargo, and airliner fuselage		0.0025–0.0032
Transport—conventional horizontal tail		0.02–0.03
Transport—conventional vertical tail		0.035–0.045
Landing gear of transport, cargo, and airliner		0.28–0.35