Add to ORKGThis thesis presents a state-space theory for the lift, drag, and all generalized forces of a deformable airfoil. Trailing-edge flap deflections are included implicitly as a special case of the general deformations. The theory allows for a thin airfoil performing small arbitrary motions with respect to a reference frame that can perform arbitrarily large translations and rotations in two dimensions. The theory accommodates a three-dimensional wake and is generalized to include dynamic stall. The equations are placed in matrix form for ease of implementation. Comparison with other theories and with experimental data verifies the theory
Because of their small size and flight regime, coupling of aerodynamics, structural dynamics, and fl...
This paper presents a geometrically exact semi-analytical approach to model the unsteady aerodynamic...
[[abstract]]This paper is to extend the authors’ previous work in 2010 to understand the perspective...
(ABSTRACT) Unsteady aerodynamic theories are essential in the analysis of bird and insect flight. Th...
In this paper, a low-order state-space adaptation of the unsteady lifting line model has been analyt...
The basic conceptions of the circulation theory of airfoils are reviewed briefly, and the mechanism ...
This paper derives linear 2nd order ordinary differential equations describ-ing the motion of a 2 di...
A state-space formulation for the aerodynamics of flapping flight is presented. The Duhamel\u27s pri...
A semi-analytical formulation based on conformal mapping is presented to predict the unsteady aerody...
This paper investigates the coupled aeroelastic and flight dynamics stability of flexible lightweigh...
216 p.The unsteady low Reynolds number aerodynamics of biomimetic airfoils and wings stands out as o...
In the aero-elastic analysis of wind turbines based on blade element theory, the need to include a m...
This thesis studies the on flow behaviour of the corrugated airfoil proposed by B. G Newman et al....
Helicopter rotor blades frequently encounter dynamic stall during normal flight condi-tions, limitin...
A numerical framework is presented to simulate rigid and flexible flapping wings. The fluid-structur...
Because of their small size and flight regime, coupling of aerodynamics, structural dynamics, and fl...
This paper presents a geometrically exact semi-analytical approach to model the unsteady aerodynamic...
[[abstract]]This paper is to extend the authors’ previous work in 2010 to understand the perspective...
(ABSTRACT) Unsteady aerodynamic theories are essential in the analysis of bird and insect flight. Th...
In this paper, a low-order state-space adaptation of the unsteady lifting line model has been analyt...
The basic conceptions of the circulation theory of airfoils are reviewed briefly, and the mechanism ...
This paper derives linear 2nd order ordinary differential equations describ-ing the motion of a 2 di...
A state-space formulation for the aerodynamics of flapping flight is presented. The Duhamel\u27s pri...
A semi-analytical formulation based on conformal mapping is presented to predict the unsteady aerody...
This paper investigates the coupled aeroelastic and flight dynamics stability of flexible lightweigh...
216 p.The unsteady low Reynolds number aerodynamics of biomimetic airfoils and wings stands out as o...
In the aero-elastic analysis of wind turbines based on blade element theory, the need to include a m...
This thesis studies the on flow behaviour of the corrugated airfoil proposed by B. G Newman et al....
Helicopter rotor blades frequently encounter dynamic stall during normal flight condi-tions, limitin...
A numerical framework is presented to simulate rigid and flexible flapping wings. The fluid-structur...
Because of their small size and flight regime, coupling of aerodynamics, structural dynamics, and fl...
This paper presents a geometrically exact semi-analytical approach to model the unsteady aerodynamic...
[[abstract]]This paper is to extend the authors’ previous work in 2010 to understand the perspective...