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Einfluss von Shock-Control-Bumps (SCBs) auf das transsonische Flatterverhalten

Otte, Jonathan (2021) Einfluss von Shock-Control-Bumps (SCBs) auf das transsonische Flatterverhalten. Bachelor's, Technische Universität Braunschweig.

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Item URL in elib:https://elib.dlr.de/147545/
Document Type:Thesis (Bachelor's)
Title:Einfluss von Shock-Control-Bumps (SCBs) auf das transsonische Flatterverhalten
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Otte, JonathanUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:15 September 2021
Refereed publication:No
Open Access:No
Status:Published
Keywords:Shock-Control Bumps, SCBs, transsonisches Flatterverhalten, Buffetschwingungen, Fluidmodes, abgelöste Strömung
Institution:Technische Universität Braunschweig
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Virtual Aircraft and  Validation
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Aeroelastic Simulation
Deposited By: Voß, Guido
Deposited On:17 Dec 2021 09:37
Last Modified:17 Dec 2021 09:37

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