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Axial and centrifugal compressor mean line flow analysis method [[electronic resource] /] / Joseph P. Veres ; prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 5-8, 2009
Axial and centrifugal compressor mean line flow analysis method [[electronic resource] /] / Joseph P. Veres ; prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 5-8, 2009
Autore Veres Joseph P
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009]
Descrizione fisica 1 online resource (32 pages) : illustrations
Collana NASA TM-
Soggetto topico Turbocompressors
Fluid flow
Computational fluid dynamics
Compressible fluids
Design analysis
Guide vanes
Centrifugal compressors
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910696924603321
Veres Joseph P  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Compressor study to meet large civil tilt rotor engine requirements [[electronic resource] /] / Joseph P. Veres ; prepared for the 65th Annual Forum and Technology Display sponsored by the American Helicopter Society, Grapevine, Texas, May 27-29, 2009
Compressor study to meet large civil tilt rotor engine requirements [[electronic resource] /] / Joseph P. Veres ; prepared for the 65th Annual Forum and Technology Display sponsored by the American Helicopter Society, Grapevine, Texas, May 27-29, 2009
Autore Veres Joseph P
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009]
Descrizione fisica 1 online resource (35 pages) : illustrations
Altri autori (Persone) HenriksenStephen
Collana NASA TM
Soggetto topico Compressors
Turbocompressors
Tilt rotor aircraft
Leading edges
Rotary wing aircraft
Engine design
Flow velocity
Centrifugal force
Trailing edges
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910697087203321
Veres Joseph P  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui