Reduced order unsteady aerodynamic model of a rigid aerofoil in gust encounters-Reference-Cited by-同舟云学术

Reduced order unsteady aerodynamic model of a rigid aerofoil in gust encounters

Published:2017-04 Issue: Volume:63 Page:203-213
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhou Qiang^ORCID,Chen Gang,Da Ronch Andrea^ORCID,Li Yueming

Funder

National Program on Key Research Projects

National Natural Science Foundation of China

Basic Research foundations for the Central Universities

Royal Academy of Engineering

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

1. L. Bensch, H. Henrichfreise, J. Jusseit, L. Merz, Method for reconstructing gusts and structural loads at aircraft, in particular passenger, aircraft, June 26 2007, US Patent 8,209,159.

2. General theory of aerodynamic instability and the mechanism of flutter;Theodorsen,1935

3. The unsteady lift of a wing of finite aspect ratio;Jones,1940

4. Unsteady lift of a flapped airfoil by indicial concepts;Leishman;J. Aircr.,1994

5. The aerodynamic force on an airfoil in a moving gust;Miles;J. Aerosp. Sci.,1956

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