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SFB880 Vehicle Concepts and Comparative Noise Assessment

Blinstrub, Jason (2019) SFB880 Vehicle Concepts and Comparative Noise Assessment. Final Symposium of the Collaborative Research Center 880, 2019-12-17 - 2019-12-18, Braunschweig.

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Official URL: https://www.tu-braunschweig.de/sfb880


The Coordinated Research Centre 880 (CRC880) focuses on the development of a new active high-lift system, which enables short take-off and landing, low fuel consumption, and low noise immission. In order to assess the active high-lift system on an aircraft level, several vehicle variants that are equipped with this active high-lift system were developed within the CRC880 over the past 9 years. This article describes the CRC880 vehicle concepts and evaluates their advantages and disadvantages in detail. Furthermore, the noise prediction methodology is described and the noise immission of the vehicle concepts is evaluated on a comparative basis. Results indicate that a propeller-driven short take-off and landing (STOL) aircraft is cost-efficient but has increased noise immission compared to a current aircraft. On the other side, STOL aircraft with turbofan engines located on top and aft of the main wing for fan sound shielding are more expensive but offer significant noise reductions.

Item URL in elib:https://elib.dlr.de/129798/
Document Type:Conference or Workshop Item (Speech)
Title:SFB880 Vehicle Concepts and Comparative Noise Assessment
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Blinstrub, JasonUNSPECIFIEDhttps://orcid.org/0000-0003-1913-0529UNSPECIFIED
Date:December 2019
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:SFB 880, aircraft design, aircraft noise, active high-lift
Event Title:Final Symposium of the Collaborative Research Center 880
Event Location:Braunschweig
Event Type:national Conference
Event Start Date:17 December 2019
Event End Date:18 December 2019
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation (old)
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Helicopter, GO
Deposited By: Winkels, Elisabeth
Deposited On:07 Jan 2020 14:56
Last Modified:24 Apr 2024 20:33

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