Numerical investigation of the influence of acceleration and deceleration on the aerodynamic characteristics of an oscillating wing aerofoil operating at transonic and hypersonic speeds
Presentation / Conference Contribution
The aerodynamic characteristics of a hypersonic aircraft are strongly influenced by the accelerating and decelerating motions of the body. This impact can be more complicated when the oscillatory motion of the body in a complex non-linear mode is inv... Read More about Numerical investigation of the influence of acceleration and deceleration on the aerodynamic characteristics of an oscillating wing aerofoil operating at transonic and hypersonic speeds.