33th Congress of the International Council of the Aeronautical Sciences

01.2 - Aircraft Design and Integrated System (Applications)

LTO NOISE AND SONIC BOOM PREDICTIONS IN EARLY CONCEPTUAL DESIGN PHASES

G. 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.


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