Experiments assessing the effectiveness of passive control involving a porous surface and cavity underneath for reducing the level of surface pressure fluctuations in reattaching flows are reported. Measurements are made on a generic axisymmetric body, representative of a launch vehicle configuration, in the Mach number range of 0.8 to 1.2. The measurements consist of distributions of mean surface pressure and unsteady surface pressure fluctuations in the boat-tail separated region. The passive control significantly reduces the peak surface pressure fluctuations in the reattachment zone, even in the absence of a strong shock wave. The spectra of pressure fluctuations reveal that with passive control the energy is appreciably reduced over a ...
In this study, a duct is considered and special attention is paid to a passive method for the contro...
The purpose of this investigation is to qualitatively explain the flow phenomena which occur on a ba...
Windtunnel tests were carried out with the aim of establishing a measured unsteady surface pressure ...
Experiments assessing the effectiveness of passive control involving a porous surface and cavity und...
The base flow of an axisymmetric generic space launcher model is investigated experimentally by mean...
Experiments were carried out investigating the features of mean and unsteady surface pressure fluctu...
Experiments were carried out investigating the mean and unsteady surface pressure fluctuations in bo...
Experiments were carried out investigating the features of mean and unsteady surface pressure fluctu...
An experimental investigation evaluating the effects of flow control on the near-wake downstream of ...
Supersonic flow over cavities has been of interest since 1960s because cavities represent the bomb b...
This work is concerned with the application of a simple passive control device with the main focus a...
The paper presents the experimental investigations on a blunt cone-cylinder made in the DLR 1- x 1-m...
During an experiment at high subsonic speeds on a two-dimensional aerofoil with a passive system for...
Experimental studies on the measurement of pressure fields in the region of separating and reattachi...
The effects of a passive control boundary layer applied around the throat on a transonic diffuser we...
In this study, a duct is considered and special attention is paid to a passive method for the contro...
The purpose of this investigation is to qualitatively explain the flow phenomena which occur on a ba...
Windtunnel tests were carried out with the aim of establishing a measured unsteady surface pressure ...
Experiments assessing the effectiveness of passive control involving a porous surface and cavity und...
The base flow of an axisymmetric generic space launcher model is investigated experimentally by mean...
Experiments were carried out investigating the features of mean and unsteady surface pressure fluctu...
Experiments were carried out investigating the mean and unsteady surface pressure fluctuations in bo...
Experiments were carried out investigating the features of mean and unsteady surface pressure fluctu...
An experimental investigation evaluating the effects of flow control on the near-wake downstream of ...
Supersonic flow over cavities has been of interest since 1960s because cavities represent the bomb b...
This work is concerned with the application of a simple passive control device with the main focus a...
The paper presents the experimental investigations on a blunt cone-cylinder made in the DLR 1- x 1-m...
During an experiment at high subsonic speeds on a two-dimensional aerofoil with a passive system for...
Experimental studies on the measurement of pressure fields in the region of separating and reattachi...
The effects of a passive control boundary layer applied around the throat on a transonic diffuser we...
In this study, a duct is considered and special attention is paid to a passive method for the contro...
The purpose of this investigation is to qualitatively explain the flow phenomena which occur on a ba...
Windtunnel tests were carried out with the aim of establishing a measured unsteady surface pressure ...