elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Aeroelastic Stability of Cylindrical Shells in Supersonic Flow with Boundary Layer

Alder, Marko (2017) Aeroelastic Stability of Cylindrical Shells in Supersonic Flow with Boundary Layer. 23rd AIAA Computational Fluid Dynamics Conference, AIAA AVIATION Forum, (AIAA 2017-3618), 5.-9. Jun. 2017, Vereinigte Staaten von Amerika. DOI: 10.2514/6.2017-3618

[img] PDF - Registered users only
2MB

Official URL: https://doi.org/10.2514/6.2017-3618


Item URL in elib:https://elib.dlr.de/115968/
Document Type:Conference or Workshop Item (Speech)
Title:Aeroelastic Stability of Cylindrical Shells in Supersonic Flow with Boundary Layer
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Alder, Markomarko.alder (at) dlr.deUNSPECIFIED
Date:June 2017
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.2514/6.2017-3618
Status:Published
Keywords:Cylinder, Flutter, Stability, Boundary Layer
Event Title:23rd AIAA Computational Fluid Dynamics Conference, AIAA AVIATION Forum, (AIAA 2017-3618)
Event Location:Vereinigte Staaten von Amerika
Event Type:international Conference
Event Dates:5.-9. Jun. 2017
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Wiederverwendbare Raumfahrtsysteme
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Spacecraft, BS
Deposited By: Alder, Marko
Deposited On:05 Dec 2017 10:59
Last Modified:05 Dec 2017 10:59

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.