An experimental investigation has been carried out on a subscale truncated ideal contour (TIC) nozzle to study the flow separation phenomena. Tests were made in the P6.2 cold gas subscale facility at DLR Lampoldshausen. Simultaneous wall pressure measurements and surface oil pigment technique was used to study the flow field features at various nozzle pressure ratios. The area-ratio of the nozzle is 20.66 and the test gas is nitrogen. Tests indicate that in a TIC nozzle the main contribution towards side-loads is the pressure pulsation of the flow in the separation region in combination with the flow asymmetry. Separation data also indicates a hyteresis in the Xinc movement during start up and shut down sequences and the circumferential 'rm...
The flow separation within convergent–divergent rocket engine nozzles induces undesired side loads. ...
This paper presents numerical and experimental findings regarding flow separation phenomenon in a hi...
As a part of an aerodynamics Ecole Polytechnique project, separation modes which occur in supersonic...
An experimental investigation has been carried out on a subscale truncated ideal contour (TIC) nozzl...
Subscale tests of nozzle flows have been performed at DLR's P6.2 test facility to investigate side-l...
An experimental investigation was conducted in a cold flow test facility to identify the origin of v...
DLR Lampoldshausen carried out cold flow tests to study the flow field in a truncated ideal contour ...
During the transient phases of start-up and shut-down, liquid engine nozzles operate under severe ov...
Abstract: An experimental investigation has been carried out to study the flow characteristics of a ...
DLR Lampoldshausen carried out cold flow subscale tests to study the wall temperature increase withi...
An experimental investigation has been carried out on a subscale thrust optimized parabolic nozzle (...
During the unsteady start-up and shut-down process in supersonic rocket engine nozzles high sideload...
Flow separation control stragies on contour bump models under a Mach 1.3 freestream has been investi...
In this paper. surface flow features such as length of separation region and separation bubble are s...
Within a joint research effort of Astrium and DLR, cold-gas test campaigns with subscale nozzles wer...
The flow separation within convergent–divergent rocket engine nozzles induces undesired side loads. ...
This paper presents numerical and experimental findings regarding flow separation phenomenon in a hi...
As a part of an aerodynamics Ecole Polytechnique project, separation modes which occur in supersonic...
An experimental investigation has been carried out on a subscale truncated ideal contour (TIC) nozzl...
Subscale tests of nozzle flows have been performed at DLR's P6.2 test facility to investigate side-l...
An experimental investigation was conducted in a cold flow test facility to identify the origin of v...
DLR Lampoldshausen carried out cold flow tests to study the flow field in a truncated ideal contour ...
During the transient phases of start-up and shut-down, liquid engine nozzles operate under severe ov...
Abstract: An experimental investigation has been carried out to study the flow characteristics of a ...
DLR Lampoldshausen carried out cold flow subscale tests to study the wall temperature increase withi...
An experimental investigation has been carried out on a subscale thrust optimized parabolic nozzle (...
During the unsteady start-up and shut-down process in supersonic rocket engine nozzles high sideload...
Flow separation control stragies on contour bump models under a Mach 1.3 freestream has been investi...
In this paper. surface flow features such as length of separation region and separation bubble are s...
Within a joint research effort of Astrium and DLR, cold-gas test campaigns with subscale nozzles wer...
The flow separation within convergent–divergent rocket engine nozzles induces undesired side loads. ...
This paper presents numerical and experimental findings regarding flow separation phenomenon in a hi...
As a part of an aerodynamics Ecole Polytechnique project, separation modes which occur in supersonic...