The complex fluid-dynamic instabilities and shock waves occurring along the surface of a
two-dimensional wedge at high values of the Mach number are studied here through …

In the present condition, there is a high demand for exact solutions through analytical,
computational and measurements in the field of aerospace engineering. For wind tunnel …

In the present study, the prime attention is to numerically simulate the surface pressure
distribution over the slant length of the cone at the various Mach numbers and for the …

This paper presents the results of an analytical study to account the effect of the sweep
angle of a delta wing whose leading edges are curved on roll damping derivative at various …

This paper presents the effect of sweep angle on a roll of damping derivative of a delta wing
with half sine wave for an attached shock case in supersonic/hypersonic flow has been …

Accurate estimation of the aerodynamic stability derivatives of airplanes is essential to
evaluate the performance of the aircraft, whether civilian or military. Theoretical prediction …

This work aims to compute stability derivatives in the Newtonian limit in pitch when the Mach
number tends to infinity. In such conditions, these stability derivatives depend on the Ogive's …

This paper focusses attention on theinfluence of prominent curvedends
torestrainingderivedowing to the transversefrequency for the numerous amplitude, flow …

In this modern era of space flight dynamics, every nation wants to share its pride in
developing one of the fastest flights and make its defense aircrafts the best. In designing the …

Stability derivatives for an ogive are obtained in the limiting case of the Mach number when
it tends to infinity. The derivative in stiffness declines with the position of pivot for the whole …