01.2 - Aircraft Design and Integrated System (Applications)LTO NOISE AND SONIC BOOM PREDICTIONS IN EARLY CONCEPTUAL DESIGN PHASESG. Piccirilloš, S. Grazianiš, R. Fusaroš, N. Violaš; šPolitecnico di Torino, Italy This paper discloses a workflow to integrate LTO noise and sonic boom predictions since the beginning of the design of future supersonic civil aircraft. The application of state-of-the-art models to future high-speed case study is discussed and solutions to overcome limitations are presented. The workflow is validated against Concorde literature data and then applied to the design of a future sustainable Mach 2 aircraft. |