Development of a Simulation Process for Conceptual CS-23 Propeller Aircraft System Noise Assessment

Conference Paper (2025)
Author(s)

K.S. Hon (Deutsches Zentrum für Luft- und Raumfahrt (DLR))

Vincent Domogalla (Deutsches Zentrum für Luft- und Raumfahrt (DLR))

Antje Feldhusen-Hoffmann (Deutsches Zentrum für Luft- und Raumfahrt (DLR))

J. Blinstrub (Deutsches Zentrum für Luft- und Raumfahrt (DLR))

Lothar Bertsch (Deutsches Zentrum für Luft- und Raumfahrt (DLR))

M. Snellen (TU Delft - Aerospace Engineering)

Thomas Zill (Deutsches Zentrum für Luft- und Raumfahrt (DLR))

Maik Angermann (Deutsches Zentrum für Luft- und Raumfahrt (DLR))

Department
Control & Operations
DOI related publication
https://doi.org/10.2514/6.2025-3365 Final published version
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Publication Year
2025
Language
English
Department
Control & Operations
Article number
AIAA 2025-3365
ISBN (electronic)
978-1-62410-738-2
Event
AIAA Aviation Forum and ASCEND 2025 (2025-07-21 - 2025-07-25), Las Vegas, United States
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Abstract

Many highly interdependent disciplines are concerned with the system noise assessment of small propeller aircraft concepts, including aircraft, propeller, engine design and acoustic modelling, flight trajectories calculation, noise propagation and ground effect modelling. There are no state-of-the-art simulation processes in Europe which account for all the aforementioned disciplines, as efforts heretofore have been focused on large transport aircraft concepts. This paper presents the development of such a simulation process at the German Aerospace Center (DLR). The simulation process inputs top-level aircraft design requirements, producing a valid CS-23 conceptual propeller aircraft design. It then calculates realistic flight paths for departure and approach for the conceptual aircraft and simulates noise immissions at user-specified locations. The immissions assessment would then guide design modifications, low-noise flight trajectory generation and novel aircraft design. A Reims-Cessna F406 is considered as the reference aircraft and is used to obtain the first results from the simulation process. The results are compared with measurements from a flight test campaign using the same aircraft. Important effects observed in the results and in the immissions assessments are also presented in this paper. Furthermore, the capabilities of the simulation chain will be demonstrated with sensitivity studies that show the effects of modifying operational procedures on ground noise immissions.

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