THE IMPACT OF VENTURI GEOMETRY ON REACTING FLOWS IN A SWIRL-VENTURI LEAN DIRECT INJECTION AIRBLAST INJECTOR (AIAA 2016-4650)
Joint propulsion conference
01.01.2016
9 pages
Aufsatz (Konferenz)
Englisch
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AIAA-2005-1106 A LEAN-DIRECT-INJECTION COMBUSTOR USING A 9 POINT SWIRL-VENTURI FUEL INJECTOR
British Library Conference Proceedings | 2005
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