Influence of flexibility on the steady aeroelastic behavior of a swept wing in transonic flow-Reference-Cited by-同舟云学术

Influence of flexibility on the steady aeroelastic behavior of a swept wing in transonic flow

Published:2018-08 Issue: Volume:81 Page:255-269
ISSN:0889-9746
Container-title:Journal of Fluids and Structures
language:en
Short-container-title:Journal of Fluids and Structures

Author:

Schewe Günter,Mai Holger

Funder

German Ministry for Education and Research and the Hermann von Helmholtz-Gemeinschaft

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference15 articles.

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4. Aerodynamischer Auftrieb bei Überschallgeschwindigkeit;Busemann;Luftfahrtforschung,1935

5. Dietz, G., Schewe, G., Kießling, F., Sinapius, M., 2003. Limit-cycle-oscillation experiments at a transport aircraft wing model. In: Int. Forum Aeroelasticity and Structural Dynamics (IFASD) Amsterdam.

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