FUEL ATOMIZATION AND DROPLET BREAKUP MODELS FOR NUMERICAL SIMULATION OF SPRAY COMBUSTION IN A SCRAMJET COMBUSTOR
18th, AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference ; 2012 ; Tours, France
2012-01-01
9 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
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Numerical simulation of angular injection of hydrogen fuel in scramjet combustor
Online Contents | 2012
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