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[null,"1.","Record Nr.",null,"UNINA9910698995003321"]
[null,null,"Autore",null,"Powell A. G"]
[null,null,"Titolo",null,"Feasibility and benefits of laminar flow control on supersonic cruise airplanes [[electronic resource] /] / A.G. Powell, S. Agrawal, T. R. Lacey"]
[null,null,"Pubbl/distr/stampa",null,"Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1989]"]
[null,null,"Descrizione fisica",null,"1 volume"]
[null,null,"Collana",null,"NASA contractor report ; ; 181817"]
[null,null,"Soggetti",null,"Aerodynamic configurations"]
[{"$nulls":4},"Boundary layer control"]
[{"$nulls":4},"Boundary layer stability"]
[{"$nulls":4},"Feasibility analysis"]
[{"$nulls":4},"Fighter aircraft"]
[{"$nulls":4},"Laminar boundary layer"]
[{"$nulls":4},"Laminar flow"]
[{"$nulls":4},"Supersonic aircraft"]
[{"$nulls":4},"Supersonic cruise aircraft research"]
[{"$nulls":4},"Supersonic transports"]
[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 Jun. 9, 2009)"]