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[null,"1.","Record Nr.",null,"UNINA9910699539803321"]
[null,null,"Autore",null,"Arrington Lynn A"]
[null,null,"Titolo",null,"Performance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydrogen/oxyen rocket [[electronic resource] /] / Lynn A. Arrington and Brian D. Reed"]
[null,null,"Pubbl/distr/stampa",null,"[Cleveland, Ohio] : , : National Aeronautics and Space Administration, Lewis Research Center, , [1992?]"]
[null,null,"Descrizione fisica",null,"1 online resource (20 pages) : digital, PDF file"]
[null,null,"Collana",null,"NASA technical memorandum ; ; 105967"]
[null,null,"Soggetti",null,"Axisymmetric flow"]
[{"$nulls":4},"Coolants"]
[{"$nulls":4},"Film cooling"]
[{"$nulls":4},"Fluid injection"]
[{"$nulls":4},"Hydrogen"]
[{"$nulls":4},"Hydrogen oxygen engines"]
[{"$nulls":4},"Propulsion system performance"]
[{"$nulls":4},"Reacting flow"]
[{"$nulls":4},"Three dimensional flow"]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,null,"Note generali","Title from title screen (viewed Aug. 25, 2010)."]
[null,null,null,"Nota di bibliografia","Includes bibliographical references (pages 8-9)."]