Design and implementation of a test bench for an aerospike nozzle allowing the visualization of compressible flow phenomena using the shadowgraph technique. The work is organized in four steps: Pre-design theoretical analysis using compressible flow theory Numerical simulations using the finite elements method with the OpenFOAM softaware Design of the nozzle and description of the pre-existing test bench Experimental results, their analysis and comparison to theory and simulation.Master [120] : ingénieur civil électromécanicien, Université catholique de Louvain, 201
The successful establishment of civil supersonic transport relies heavily on reducing sonic boom sig...
Shadowgraph techniques were applied to the cold flow ejector facility at the Propulsion Research Cen...
The paper presents development of a low-fidelity tool capable of calculating pressure and velocity f...
A total of 142 shadowgraph photographs were taken on 43 different plumes that were distributed over ...
Abstract This paper will be describing the effects of operating altitude of aerospike nozzle to its ...
A novel shadowgraph flow visualisation technique has been developed and used to visualise key region...
A system for cold flow testing of an aerospike nozzle has been developed in an effort to examine the...
An apparatus was designed and constructed to study supersonic fluid flow in a low temperature and lo...
The present study involves the shock wave and consequent vortex loop generated when a shock tube wit...
This report describes the progress of work done in the project "Experimental study on conical aerosp...
Aerospike nozzles possess many qualities that make them more desirable and efficient than convention...
The paper reports flow visualizations of a free slot jet of air, obtained with the shadowgraph techn...
In present work a test rig for cold flow test experiments on linear aerospike nozzles has been desig...
At the preliminary design stage for an aero-engine, the evaluation of the nozzle performance is an i...
Shadowgraph photography techniques in transonic wind tunnel tests are described. The system was used...
The successful establishment of civil supersonic transport relies heavily on reducing sonic boom sig...
Shadowgraph techniques were applied to the cold flow ejector facility at the Propulsion Research Cen...
The paper presents development of a low-fidelity tool capable of calculating pressure and velocity f...
A total of 142 shadowgraph photographs were taken on 43 different plumes that were distributed over ...
Abstract This paper will be describing the effects of operating altitude of aerospike nozzle to its ...
A novel shadowgraph flow visualisation technique has been developed and used to visualise key region...
A system for cold flow testing of an aerospike nozzle has been developed in an effort to examine the...
An apparatus was designed and constructed to study supersonic fluid flow in a low temperature and lo...
The present study involves the shock wave and consequent vortex loop generated when a shock tube wit...
This report describes the progress of work done in the project "Experimental study on conical aerosp...
Aerospike nozzles possess many qualities that make them more desirable and efficient than convention...
The paper reports flow visualizations of a free slot jet of air, obtained with the shadowgraph techn...
In present work a test rig for cold flow test experiments on linear aerospike nozzles has been desig...
At the preliminary design stage for an aero-engine, the evaluation of the nozzle performance is an i...
Shadowgraph photography techniques in transonic wind tunnel tests are described. The system was used...
The successful establishment of civil supersonic transport relies heavily on reducing sonic boom sig...
Shadowgraph techniques were applied to the cold flow ejector facility at the Propulsion Research Cen...
The paper presents development of a low-fidelity tool capable of calculating pressure and velocity f...