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Flutter assessment of DLR-D150-Vamp configuration w.r.t. UHBR engine integration

Neumann, Jens (2020) Flutter assessment of DLR-D150-Vamp configuration w.r.t. UHBR engine integration. DLR-Interner Bericht. DLR-IB-AE-GO-2020-106. 107 S.

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Abstract

This report presents comprehensive flutter calculations of the DLR-D150-VAMP configuration with respect to the influence of structural changes on flutter behaviour. The main focus thereby was on the influence of modifications concerning the position of the engines/nacelles. Furthermore the influence of gyroscopic and thrust vector effects as well as the influence of pylon stiffness regarding the flutter behaviour has been investigated. Finally, the influence of an integrated ultra high bypass ratio engine/nacelle (UHBR) instead of a classical standard CFM56 engine on the flutter stability has been investigated. The results are shown in comparison to the aeroelastic flight envelope for this assessed configuration, which is similar to an A320 aircraft.

Item URL in elib:https://elib.dlr.de/139635/
Document Type:Monograph (DLR-Interner Bericht)
Title:Flutter assessment of DLR-D150-Vamp configuration w.r.t. UHBR engine integration
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Neumann, JensInstitut für AeroelastikUNSPECIFIEDUNSPECIFIED
Date:August 2020
Refereed publication:No
Open Access:No
Number of Pages:107
Status:Published
Keywords:aeroelasticity, flutter, UHBR engine integration, DLR-D150-Vamp
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:air traffic management and operations
DLR - Research area:Aeronautics
DLR - Program:L AO - Air Traffic Management and Operation
DLR - Research theme (Project):L - Human factors and safety in Aeronautics (old)
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: Neumann, Jens
Deposited On:22 Dec 2020 15:38
Last Modified:25 Jan 2021 15:14

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