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), 2017-06-05 - 2017-06-09, Vereinigte Staaten von Amerika. doi: 10.2514/6.2017-3618.

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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:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Alder, Marko	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

June 2017

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

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 Start Date:

5 June 2017

Event End Date:

9 June 2017

Organizer:

AIAA

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Space

HGF - Program Themes:

Space Transportation

DLR - Research area:

Raumfahrt

DLR - Program:

R RP - Space Transportation

DLR - Research theme (Project):

R - Wiederverwendbare Raumfahrtsysteme (old)

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:

24 Apr 2024 20:20

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