The unsteadiness of the bow-shock wave in front of a 7-inch diameter Apollo-shaped capsule was measured in the T5 hypervelocity shock tunnel at GALCIT. The pressure fluctuations in the reservoir generate expansion and compression waves traveling down the nozzle which interact with the bow-shock in front of the model. The resulting bow-shock displacement is measured using a high-speed Schlieren system where the shock position is extracted using a sub-pixel tracking algorithm. Oscillations of the shock position with amplitudes between ±1% to ±5% of the standoff distance are measured. The power spectrum of the bow-shock motion displays frequencies in the 10 kHZ range corresponding to the frequency content of the pressure fluctuations measured ...
The unsteady characteristics of the second throat of a transonic wind tunnel have an important influ...
The presented research investigates the effects of shock wave boundary layer interaction on the unst...
Fundamental experiments were performed in an unsteady flow water table facility to investigate and q...
The unsteadiness of the bow-shock wave in front of a 7-inch diameter Apollo-shaped capsule was measu...
This manuscript presents mechanisms to explain and mathematics to model time-averaged spatially-reso...
The character of the boundary layer noise and ambient tunnel noise are of interest in the experiment...
The flow field in a hypersonic inlet model at a design point of M = 6 has been studied experimentall...
Experiments on shock-wave/boundary-layer interaction of an impinging shock on a flat panel at Mach n...
An analytical investigation is performed to study the unsteady response of a one-dimensional, non-li...
AbstractPressure sensing and schlieren imaging with high resolution and sensitivity are applied to t...
The phenomena of self-sustained shock wave oscillations over conical bodies with a blunt axisymmetri...
Transonic shock wave/boundary layer interaction over a wall-mounted bump was investigated with speci...
Transition from laminar to turbulent flow in hypersonic boundary layers leads to highly elevated lev...
Pressure sensing and schlieren imaging with high resolution and sensitivity are applied to the study...
A new method to measure shock wave unsteadiness is presented. Time-resolved visualizations of the fl...
The unsteady characteristics of the second throat of a transonic wind tunnel have an important influ...
The presented research investigates the effects of shock wave boundary layer interaction on the unst...
Fundamental experiments were performed in an unsteady flow water table facility to investigate and q...
The unsteadiness of the bow-shock wave in front of a 7-inch diameter Apollo-shaped capsule was measu...
This manuscript presents mechanisms to explain and mathematics to model time-averaged spatially-reso...
The character of the boundary layer noise and ambient tunnel noise are of interest in the experiment...
The flow field in a hypersonic inlet model at a design point of M = 6 has been studied experimentall...
Experiments on shock-wave/boundary-layer interaction of an impinging shock on a flat panel at Mach n...
An analytical investigation is performed to study the unsteady response of a one-dimensional, non-li...
AbstractPressure sensing and schlieren imaging with high resolution and sensitivity are applied to t...
The phenomena of self-sustained shock wave oscillations over conical bodies with a blunt axisymmetri...
Transonic shock wave/boundary layer interaction over a wall-mounted bump was investigated with speci...
Transition from laminar to turbulent flow in hypersonic boundary layers leads to highly elevated lev...
Pressure sensing and schlieren imaging with high resolution and sensitivity are applied to the study...
A new method to measure shock wave unsteadiness is presented. Time-resolved visualizations of the fl...
The unsteady characteristics of the second throat of a transonic wind tunnel have an important influ...
The presented research investigates the effects of shock wave boundary layer interaction on the unst...
Fundamental experiments were performed in an unsteady flow water table facility to investigate and q...