This module will consider mission-based subsonic aircraft design methodology: Weight estimation, sensitivity analysis, take-off, and landing performance, Bréguet range equation for turbofan aircraft and piston engines/turboprop aircraft. It will cover aerodynamic design: subsonic-supersonic compatibility, wing and body design, supersonic drag and area ruling, sonic boom, radiation, take-off noise. It will also consider air-breathing Engine Design and Noise in Propeller and jet-driven aeroplanes including performance calculations and new developments in electric propulsion and other concepts of propulsion.

Lists linked to Conceptual Design of Aircraft

Title Sort by title Year Last updated Sort by last updated
EMS611U (&DENM305) Conceptual design of aircraft 2023-2024 Academic Year 17/09/2023 19:44:35
EMS611U (&DENM305) Conceptual design of aircraft 2024-2025 Academic Year 13/06/2024 12:31:53