The interaction between active aeroelastic control and structural tailoring in aeroservoelastic wing design-Reference-Cited by-同舟云学术

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The interaction between active aeroelastic control and structural tailoring in aeroservoelastic wing design

Published:2021-03 Issue: Volume:110 Page:106516
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Binder Simon,Wildschek Andreas^ORCID,De Breuker Roeland

Funder

Technische Universiteit Delft

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference49 articles.

1. Airbus airframe – new technologies and management aspects;Rösner;Materialwissenschaft und Werkstofftechnik,2006

2. M.M. Munk, Laminated propeller, U.S. patent no. 2,599,718, 1949.

3. Aeroelastic tailoring - theory, practice, and promise;Shirk;J. Aircr.,1986

4. Aeroelastic tailoring - creative uses of unusual materials;Weisshaar,1987

5. Optimal design of composite wing subjected to gust loads;Kim;Comput. Struct.,2005

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2. An equivalent emulation method of gust response for flight tests;Aerospace Science and Technology;2023-11

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