Flutter is the phenomenon where the body will experience uncontrolled motions after reaching a certain velocity known as the critical velocity. The focus of this work is on studying the influence of position of camber of an airfoil on its flutter behaviour. Four different NACA five digit airfoils were selected based on the variation in position of camber and were analyzed at different air speeds. These airfoils were studied for their pitch and plunge behaviour which are the base for understanding the flutter characteristics of any body and the flutter characteristics are derived from those results
The effects of unequal pitching and plunging frequency on the flow structures around a flapping airf...
A solution procedure is described for determining the two-dimensional and two-degrees of freedom flu...
An experimental investigation is presented for the aeroelastic response of a two-degree-of-freedom ...
The problem of flutter is first introduced. The equations of motion of an airfoil with two degrees o...
Abstract. This paper numerically investigates the effect of chordwise flexibility on the stability o...
This report contains the results of a series of tests on the flexure-torsion flutter of cascades of ...
The problem of unsteady aerodynamic interference between n interfering bodies or surfaces is solved ...
The results of the basic flutter theory originally devised in 1934 and published as NACA Technical R...
In this thesis the torsional-flexural response of a two-dimensional airfoil to forced oscillations o...
Some of the other factors considered were found to be more or less significant however, all the fact...
In this work, flutter behaviour of NACA 6409 is investigated using wind tunnel. The plunging and pit...
An experimental investigation was made of a preloaded spring-tab flutter model to determine the effe...
This paper is concerned with a discussion of some of the problems of flutter and aeroelasticity that...
AbstractEvery object has its own natural frequency when the frequency of a source is equal to the ob...
This paper derives linear 2nd order ordinary differential equations describ-ing the motion of a 2 di...
The effects of unequal pitching and plunging frequency on the flow structures around a flapping airf...
A solution procedure is described for determining the two-dimensional and two-degrees of freedom flu...
An experimental investigation is presented for the aeroelastic response of a two-degree-of-freedom ...
The problem of flutter is first introduced. The equations of motion of an airfoil with two degrees o...
Abstract. This paper numerically investigates the effect of chordwise flexibility on the stability o...
This report contains the results of a series of tests on the flexure-torsion flutter of cascades of ...
The problem of unsteady aerodynamic interference between n interfering bodies or surfaces is solved ...
The results of the basic flutter theory originally devised in 1934 and published as NACA Technical R...
In this thesis the torsional-flexural response of a two-dimensional airfoil to forced oscillations o...
Some of the other factors considered were found to be more or less significant however, all the fact...
In this work, flutter behaviour of NACA 6409 is investigated using wind tunnel. The plunging and pit...
An experimental investigation was made of a preloaded spring-tab flutter model to determine the effe...
This paper is concerned with a discussion of some of the problems of flutter and aeroelasticity that...
AbstractEvery object has its own natural frequency when the frequency of a source is equal to the ob...
This paper derives linear 2nd order ordinary differential equations describ-ing the motion of a 2 di...
The effects of unequal pitching and plunging frequency on the flow structures around a flapping airf...
A solution procedure is described for determining the two-dimensional and two-degrees of freedom flu...
An experimental investigation is presented for the aeroelastic response of a two-degree-of-freedom ...