01.2 - Aircraft Design and Integrated System (Applications)
DESIGN OF THE SENECA MACH 1.8 SUPERSONIC AIRLINER WITH MULTI-FIDELITY AERODYNAMIC ANALYSIS FOR NOISE-OPTIMISED TAKE-OFF TRAJECTORIES
C. Villena Muñoz¹, C. Lawson¹, A. Riaz¹, A. Sharma¹; ¹Cranfield University, United Kingdom
SENECA advances multi-disciplinary optimisation for sustainable supersonic aircraft, focusing on noise reduction, emission levels, fuel efficiency, and low drag. The project proposes MDO for a Mach 2.2 supersonic airliner, assessing various configurations with different fidelity levels methods. Trade-off studies contribute to a comprehensive description and analysis, enhancing data reliability.