Aeroelastic analysis for flap of airfoil in transonic flow

Author:

Yang S.,Lee I.

Publisher

Elsevier BV

Subject

Computer Science Applications,Mechanical Engineering,General Materials Science,Modelling and Simulation,Civil and Structural Engineering

Reference16 articles.

1. Current status of computational methods for transonic unsteady aerodynamics and aeroelastic applications;Edwards;NASA TM 104191,1991

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

3. The transonic oscillating flap;Magnus,1976

4. Implicit finite-difference computations of unsteady transonic flows about airfoils;Ballhaus;AIAA J.,1977

5. Transonic time-response analysis of three degrees of freedom conventional and supercritical airfoils;Yang,1982

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1. Stalling angle predictions of symmetric aero foil by flow analysis;2ND INTERNATIONAL CONFERENCE ON ADVANCED RESEARCH IN MECHANICAL ENGINEERING (2ND ICARME – 21);2022

2. Influence of aeroelastic control reversal problem in the airplane lateral stability modes;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2014-05-29

3. Improving the Aeroelastic Flutter Characteristics of Supersonic Beams Using Piezoelectric Material;Journal of Intelligent Material Systems and Structures;2011-04-13

4. Numerical modelling of aeroelastic behaviour of an airfoil in viscous incompressible flow;Applied Mathematics and Computation;2011-02

5. Nonlinear aeroelastic analysis of a two-dimensional wing with control surface in supersonic flow;Acta Mechanica Sinica;2010-01-10

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