A minimum objective function trim procedure for VTOLs noise reduction-Reference-Cited by-同舟云学术

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A minimum objective function trim procedure for VTOLs noise reduction

Published:2024-04 Issue: Volume:147 Page:109004
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Poggi Caterina^ORCID,Bernardini Giovanni,Gennaretti Massimo^ORCID

Publisher

Elsevier BV

Reference33 articles.

1. A review of current technology and research in urban on-demand air mobility applications;Polaczyk,2019

2. Controllability analysis for multirotor helicopter rotor degradation and failure;Du;J. Guid. Control Dyn.,2015

3. Guidance on the balanced approach to aircraft noise management;I.C.A. Organization,2008

4. Gradient-based propeller optimization with acoustic constraints;Ingraham,2019

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1. Synchrophasing control of multiple propellers based on hardware in the loop experimental platform;Aerospace Science and Technology;2024-10

2. Aeroacoustics research in Europe: The CEAS-ASC report on 2023 highlights;Journal of Sound and Vibration;2024-09

3. Low-emission optimization control method for coaxial compound helicopter/engine based on variable geometry adjustment;Aerospace Science and Technology;2024-08

4. A Minimum Objective Function Trim Procedure for VTOL Boundary Layer Trailing Edge Broadband Noise Reduction;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30

5. Aeroacoustics Research in Europe: The Ceas-Asc Report on 2023 Highlights;2024

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