The Aircraft Noise Simulation Working Group (ANSWr) – V2 Aircraft Results
THE AIRCRAFT NOISE SIMULATION WORKING GROUP (ANSWR) — V2 AIRCRAFT RESULTS
System Noise Assessment of a Tube-and-wing Aircraft with Geared Turbofan Engines (AIAA 2018-0264)
Towards an Impact-Based Noise Reduction Method for Conceptual Aircraft Design
Flight testing of noise abating required navigation performance procedures and steep approaches
Flight testing of noise abating required navigation performance procedures and steep approaches
The Parametric Aircraft Noise Analysis Module - status overview and recent applications