Investigation on flutter stability of the DLR-F19/SACCON configuration-Reference-Cited by-同舟云学术

Investigation on flutter stability of the DLR-F19/SACCON configuration

Published:2019-10 Issue: Volume:93 Page:105320
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Voss Guido,Schaefer Dominik,Vidy Cyrille

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference23 articles.

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2. Aeroelastic optimization study based on X-56A model;Li,2014

3. M. Galle, Ein Verfahren zur numerischen Simulation kompressibler, reibungsbehafteter Strömungen auf hybriden Netzen, Diss., DLR-FB, pp. 99-04, 1999.

4. Calculations of Complex Three-Dimensional Configurations Employing the DLR-TAU-Code;Gerhold,1997

5. A. Voss, T. Klimmek, Design and sizing of a parametric structural model for a UCAV configuration for loads and aeroelastic analysis, in: Deutscher Luft- und Raumfahrtkongress, 2015.

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