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Acoustic performance of novel fan noise reduction technologies for a high bypass model turbofan at simulated flight conditions [[electronic resource] /] / David M. Elliott, Richard P. Woodward, and Gary G. Podboy ; prepared for the 15th Aeroacoustics Conference (30th Aeroacoustics Conference) cosponsored by AIAA and CEAS Miami, Florida, May 11-13, 2009
Acoustic performance of novel fan noise reduction technologies for a high bypass model turbofan at simulated flight conditions [[electronic resource] /] / David M. Elliott, Richard P. Woodward, and Gary G. Podboy ; prepared for the 15th Aeroacoustics Conference (30th Aeroacoustics Conference) cosponsored by AIAA and CEAS Miami, Florida, May 11-13, 2009
Autore Elliott David M
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Descrizione fisica 1 online resource (20 pages) : illustrations
Altri autori (Persone) WoodwardRichard P
PodboyGary G
Collana NASA TM-
Soggetto topico Acoustic properties
Aerodynamic noise
Turbofans
Noise reduction
Bypass ratio
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910699547903321
Elliott David M  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor / / Richard F. Bozak, Christopher E. Hughes, James Buckley
The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor / / Richard F. Bozak, Christopher E. Hughes, James Buckley
Autore Bozak Richard F.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2013
Descrizione fisica 1 online resource (8 pages) : illustrations (some color)
Collana NASA/TM
Soggetto topico Acoustic properties
Aerodynamic noise
Blade tips
Oscillating flow
Pressure ratio
Turbofans
Rotors
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705296503321
Bozak Richard F.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Effects of inlet distortion on aeromechanical stability of a forward-swept high-speed fan [[electronic resource] /] / Gregory P. Herrick ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010
Effects of inlet distortion on aeromechanical stability of a forward-swept high-speed fan [[electronic resource] /] / Gregory P. Herrick ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010
Autore Herrick Gregory Paul <1972->
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011]
Descrizione fisica 1 online resource (14 pages) : color illustrations
Collana NASA/TM
Soggetto topico Aeroelasticity
Turbomachinery
Turbofans
Computational fluid dynamics
Inlet flow
Aerodynamic characteristics
High speed
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910700302303321
Herrick Gregory Paul <1972->  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Energy efficient engine low pressure subsystem flow analysis / / Edward J. Hall [and three others]
Energy efficient engine low pressure subsystem flow analysis / / Edward J. Hall [and three others]
Autore Hall Edward J.
Pubbl/distr/stampa [Cleveland, Ohio?] : , : National Aeronautics and Space Administration, Lewis Research Center, , April 1998
Descrizione fisica 1 online resource (xv, 159 pages) : illustrations
Collana NASA/CR
Soggetto topico Turbofan engines
Turbofans
Aerodynamic characteristics
Rotor aerodynamics
Mathematical models
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910709639903321
Hall Edward J.  
[Cleveland, Ohio?] : , : National Aeronautics and Space Administration, Lewis Research Center, , April 1998
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Fission surface power technology development status [[electronic resource] /] / Donald T. Palac ... [and others] ; prepared for the Space 2009 Conference and Exposition sponsored by the American Institute of Aeronautics and Astronautics Pasadena, California, September 14-17, 2009
Fission surface power technology development status [[electronic resource] /] / Donald T. Palac ... [and others] ; prepared for the Space 2009 Conference and Exposition sponsored by the American Institute of Aeronautics and Astronautics Pasadena, California, September 14-17, 2009
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Descrizione fisica 1 online resource (9 pages) : illustrations
Altri autori (Persone) PalacDonald T
Collana NASA TM-
Soggetto topico Acoustic properties
Aerodynamic noise
Turbofans
Noise reduction
Bypass ratio
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910699547503321
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Flutter analysis of a transonic fan / / R. Srivastava [and three others]
Flutter analysis of a transonic fan / / R. Srivastava [and three others]
Autore Srivastava R.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2002
Descrizione fisica 1 online resource (8 pages) : color illustrations
Collana NASA/TM
Soggetto topico Aeroelasticity
Flutter analysis
Transonic flow
Turbofans
Aerodynamic configurations
Scale models
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705667903321
Srivastava R.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2002
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Investigation of exoskeletal engine propulsion system concept [[electronic resource] /] / Joseph M. Roche ... [and others]
Investigation of exoskeletal engine propulsion system concept [[electronic resource] /] / Joseph M. Roche ... [and others]
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2005]
Descrizione fisica 1 online resource (88 pages) : illustrations (some color)
Altri autori (Persone) RocheJoseph M
Collana NASA/TM
Soggetto topico Propulsion system configurations
Turbofans
Gas turbine engines
Turbine blades
Compressor blades
Aerothermodynamics
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910701253503321
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2005]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Noise generation by fans with supersonic tip speeds [[electronic resource] /] / Stewart Glegg
Noise generation by fans with supersonic tip speeds [[electronic resource] /] / Stewart Glegg
Autore Glegg Stewart
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2003]
Descrizione fisica 1 online resource (7 pages) : color illustrations
Collana NASA/CR
Soggetto topico Noise generators
Turbofans
Sound waves
Stator blades
Acoustic propagation
Aerodynamic noise
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910701385703321
Glegg Stewart  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2003]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Perceived noise analysis for offset jets applied to commerical supersonic aircraft / / Dennis L. Huff [and three others]
Perceived noise analysis for offset jets applied to commerical supersonic aircraft / / Dennis L. Huff [and three others]
Autore Huff Dennis L.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , February 2019
Descrizione fisica 1 online resource (15 pages) : color illustrations
Collana NASA/TM
Soggetto topico Supersonic aircraft
Multiphase flow
Pressure ratio
Noise prediction
Turbofans
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910711967203321
Huff Dennis L.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , February 2019
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Performance and weight estimates for an advanced open rotor engine / / Eric S. Hendricks and Michael T. Tong
Performance and weight estimates for an advanced open rotor engine / / Eric S. Hendricks and Michael T. Tong
Autore Hendricks Eric S.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2012
Descrizione fisica 1 online resource (13 pages) : illustrations (some color)
Collana NASA/TM
Soggetto topico Contrarotating propellers
Performance prediction
Fuel consumption
Turbofans
Fixed wings
Mechanical drives
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702485503321
Hendricks Eric S.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2012
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui