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[null,"1.","Record Nr.",null,"UNINA9910702682503321"]
[null,null,"Autore",null,"Sanders Bobby W."]
[null,null,"Titolo",null,"Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients / / Bobby W. Sanders"]
[null,null,"Pubbl/distr/stampa",null,"Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Office, , January 1980"]
[null,null,"Descrizione fisica",null,"1 online resource (iii, 98 pages) : illustrations"]
[null,null,"Collana",null,"NASA technical paper ; ; 1531"]
[null,null,"Soggetti",null,"Airplanes - Turbojet engines - Air intakes"]
[{"$nulls":4},"Airplanes - Motors - Valves"]
[{"$nulls":4},"Aerodynamic stability"]
[{"$nulls":4},"Bypasses"]
[{"$nulls":4},"Propulsion system performance"]
[{"$nulls":4},"Supersonic inlets"]
[{"$nulls":4},"Turbojet engines"]
[{"$nulls":4},"Wind tunnel stability tests"]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,null,"Note generali","Title from title screen (viewed Sept. 22, 2014)."]
[{"$nulls":4},"\"January 1980.\""]
[{"$nulls":4},"\"Performing organization, Lewis Research Center\"--Technical report documentation page."]
[null,null,null,"Nota di bibliografia","Includes bibliographical references (pages 27-28)."]