Active aeroelastic control over a four control surface wing model-Reference-Cited by-同舟云学术

Active aeroelastic control over a four control surface wing model

Published:2009-10 Issue:7 Volume:13 Page:374-382
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Cavagna L.,Ricci S.,Scotti A.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference26 articles.

1. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows;Albano;AIAA Journal,1969

2. Unsteady Euler airfoil solution using unstructured dynamic meshes;Batina;AIAA Journal,1990

3. A procedure for tetrahedral boundary layer mesh generation;Bottasso;Engineering with Computers,2002

4. Application of Navier–Stokes simulations for aeroelastic assessment in transonic regime;Cavagna;Computers & Structures,2007

5. L. Cavagna, G. Quaranta, P. Mantegazza, D. Marchetti, Aeroelastic assessment of the free flying aircraft in transonic regime, in: International Forum on Aeroelasticity and Structural Dynamics IFASD-2007, Stockholm, Sweden, June 18–20, 2007

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