What is it about?
This work presents the modeling and assessment of noise reducing capabilities of a Blended Wing Body (BWB) aircraft compared to tube and wing aircraft in different approach and departure procedures and engine thrust capabilities. Noise reducing features of the demonstration aircraft, a vehicle representative of the state of the art JetZero BWB, are highlighted.
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This page is a summary of: Flight Procedural Noise Assessment of Blended-Wing–Body Aircraft with Variable Thrust, Journal of Aircraft, February 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c037984.
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