A multi-fidelity, multi-disciplinary analysis and optimization framework for the design of morphing UAV wing

Conference paper (2015)

Authors

A Ciarella External organisation

C Tsotskas External organisation

P Tsoutsanis External organisation

D Drikakis External organisation

M Hahn External organisation

N.P.M. Werter Aerospace Structures & Computational Mechanics - Aerospace Engineering

R. De Breuker Aerospace Structures & Computational Mechanics - Aerospace Engineering

C.S. Beaverstock External organisation

M.I. Friswell External organisation

Y. Yang External organisation

S Ozgen External organisation

A Antoniadis External organisation

Research Group

Aerospace Structures & Computational Mechanics (Aerospace Engineering) (TU Delft)

More Info

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To reference this document use:

http://resolver.tudelft.nl/uuid:98d4cb0f-f931-4ae0-ac64-98d38fc2ff53

Published Date

2015

Language

English

Reuse Rights

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Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Aerospace Structures & Computational Mechanics