Performance on the Design of Aircraft with Laminar Flow Technology

摘要: cases have to be considered already in preliminary design synthesis for correct sizing of the aircraft. In scope this paper, an approach is presented that incorporates o-design laminar aircraft into synthesis. The authors chose use extended-range twin-engine performance standards (ETOPS) as framework deriving operational with technology. Dierent requirements minimum are derived directly impact overall a case study, sensitivities towards these odesign discussed. Design parameters such maximum take-o weight, block fuel, well economics used evaluation dierent concepts.