A Hierarchical Aeroelastic Engine for the Preliminary Design and Optimization of the Flexible Aircraft-Reference-Cited by-同舟云学术

A Hierarchical Aeroelastic Engine for the Preliminary Design and Optimization of the Flexible Aircraft

Published:2013-04-05 Issue: Volume: Page:
ISSN:
Container-title:54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Ciampa Pier Davide¹,Zill Thomas¹,Nagel Bjoern¹

Affiliation:

1. German Aerospace Center (DLR)

Publisher

American Institute of Aeronautics and Astronautics

Reference32 articles.

1. 3La Rocca, G. "Knowledge Based Engineering Techniques to Support Aircraft Design and Optimization", Ph.D. Dissertation, Faculty ofAerospace Engineering,TUDelft, theNetherlands, 2011.

2. 4WrightJ.R.,andCooper,J.E,IntroductiontoAircraftAeroelasticityandLoads,AIAAEducationSeries,2007.

3. 5Howe,D.,AircraftLoadingandStructuralLayout,AIAAEducationSeries,2004.

4. Non-linear aeroelastic prediction for aircraft applications

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