Inlet Geometry Effects on the Flowfield of a Ducted Rocket Combustor
53rd, Israel annual conference on aerospace sciences ; 2013 ; Tel-Aviv, Israel
2013-01-01
17 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
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Inlet Geometry and Equivalence Ratio Effects on Combustion in a Ducted Rocket
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