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45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
The motivation for the present work came from a study on spray characteristics of cryogenic injectors where the spray did not lend itself to probing by conventional diagnostic tools. The work was later extended to gas-liquid type of impinging jet as a possible replacement to shear coaxial atomizers currently employed in cryogenic rocket engines with the attendant drawback of design and manufacturing complexity. In addition to simplicity of design and manufacture, the impinging configurationdoi:10.2514/6.2009-5392 fatcat:wwb2dgictnfcdgueydhbwwfe24