The flow field in a two-dimensional three-ramp hypersonic mixed-compression inlet in a
freestream Mach number of M∞= 5 is numerically solved to understand the unsteady …

The impinging shock of varying strengths on the free shear layer in a confined supersonic
cavity flow is studied numerically using the detached eddy simulation. The resulting …

Control surface deployment in a supersonic flow has many applications, including flow
control, mixing, and body-force regulation. The extent of control surface deflections …

The influence of the outflow initial parameters (stagnation pressure P 0 and temperature T 0,
as well as the residual pressure in the background medium P∞) on the radii in the maximum …

The paper gives experimental observations of the hypersonic flow past an axisymmetric flat-
face cylinder with a protruding sharp-tip spike. Unsteady pressure measurements and high …

A series of reduced-order numerical simulations on a specific bluff body type (v-gutters) in a
subsonic duct flow is performed to assess the unsteady wake dynamics. Two of the v-gutter's …

Unsteady flows past a spiked body are investigated numerically with wall-resolved large-
eddy simulation (LES). The inflow features a Mach number of M a= 2. 21 and a Reynolds …

In this paper, unsteady flow pulsation over four types of spiked-blunt body model and related
pulsation suppression methods are investigated through wind tunnel experiments. Direct …

Flow unsteadiness over four types of spiked-blunt body are investigated through wind tunnel
experiments at a freestream Mach number of 2.2 at 0° and 4° angle of attack. The flow …

Experiments and computations were made at a Mach number of 2.0 on a hemispherical
blunt nose body with a conical spike of L/D ratio= 1.0. Attempts were made to alter the …