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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
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Broadband shock noise in internally-mixed dual-stream jets [[electronic resource] /] / James E. Bridges ; prepared for the 15th Aeroacoustics Conference (30th AIAA Aeroacoustics Conference) cosponsored by AIAA and CEAS, Miami, Florida, May 11-13, 2009
| Broadband shock noise in internally-mixed dual-stream jets [[electronic resource] /] / James E. Bridges ; prepared for the 15th Aeroacoustics Conference (30th AIAA Aeroacoustics Conference) cosponsored by AIAA and CEAS, Miami, Florida, May 11-13, 2009 |
| Autore | Bridges James E |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009] |
| Descrizione fisica | 1 online resource (17 pages) : illustrations |
| Collana | NASA TM- |
| Soggetto topico |
Aerodynamic noise
Nozzle flow Noise measurement Flow noise Shock waves Bypass ratio Shear layers |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910696929403321 |
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Bridges James E
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Control design for an advanced geared turbofan engine / / Jeffryes W. Chapman, Jonathan S. Litt
| Control design for an advanced geared turbofan engine / / Jeffryes W. Chapman, Jonathan S. Litt |
| Autore | Chapman Jeffryes W. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , November 2017 |
| Descrizione fisica | 1 online resource (14 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Controllers
Bypass ratio Turbofan engines Flight envelopes Nonlinearity |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706533203321 |
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Chapman Jeffryes W.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , November 2017 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan / / Christopher E. Hughes, John A. Gazzaniga
| Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan / / Christopher E. Hughes, John A. Gazzaniga |
| Autore | Hughes Christopher E. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Langley Research Center, , November 2013 |
| Descrizione fisica | 1 online resource (22 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aircraft performance
Bypass ratio Fan blades Fixed wings Low speed wind tunnels Noise reduction |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702436203321 |
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Hughes Christopher E.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Langley Research Center, , November 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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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 | ||
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Fuel flexible combustor for high-OPR compact-core N+3 propulsion engine : final technical report / / Lance L. Smith
| Fuel flexible combustor for high-OPR compact-core N+3 propulsion engine : final technical report / / Lance L. Smith |
| Autore | Smith Lance L. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , March 2020 |
| Descrizione fisica | 1 online resource (91 pages) : illustrations (mostly color) |
| Collana | NASA/CR |
| Soggetto topico |
Bypass ratio
Computational fluid dynamics Combustion chambers High pressure Dynamic tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Fuel flexible combustor for high-OPR compact-core N+3 propulsion engine |
| Record Nr. | UNINA-9910713066703321 |
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Smith Lance L.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , March 2020 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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HYTESS, a Hypothetical Turbofan Engine Simplified Simulation / / Walter C. Merrill [and four others]
| HYTESS, a Hypothetical Turbofan Engine Simplified Simulation / / Walter C. Merrill [and four others] |
| Autore | Merrill Walter C. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , January 1984 |
| Descrizione fisica | 1 online resource (17 pages, 5 unnumbered pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Bypass ratio
Computerized simulation Turbofan engines FORTRAN Mathematical models User manuals (computer programs) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702516903321 |
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Merrill Walter C.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , January 1984 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Inlet acoustic data from a high bypass ratio turbofan rotor in an internal flow component test facility / / Richard F. Bozak
| Inlet acoustic data from a high bypass ratio turbofan rotor in an internal flow component test facility / / Richard F. Bozak |
| Autore | Bozak Richard F. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , May 2017 |
| Descrizione fisica | 1 online resource (6 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Acoustic properties
Aerodynamic characteristics Bypass ratio Noise reduction Rotors Turbofan engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705713903321 |
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Bozak Richard F.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , May 2017 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Jet noise scaling in dual stream nozzles [[electronic resource] /] / Abbas Khavaran, James Bridges ; prepared for the 16th Aeroacoustics Conference cosponsored by the American Institute of Aeronautics and Astronautics and the Confederation of European Aerospace Societies, Stockholm, Sweden, June 7-9, 2010
| Jet noise scaling in dual stream nozzles [[electronic resource] /] / Abbas Khavaran, James Bridges ; prepared for the 16th Aeroacoustics Conference cosponsored by the American Institute of Aeronautics and Astronautics and the Confederation of European Aerospace Societies, Stockholm, Sweden, June 7-9, 2010 |
| Autore | Khavaran Abbas <1953-> |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
| Descrizione fisica | 1 online resource (18 pages) : color illustrations |
| Altri autori (Persone) | BridgesJames |
| Collana | NASA/TM |
| Soggetto topico |
Jet aircraft noise
Aerodynamic noise Noise generators Bypass ratio High frequencies |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910700389203321 |
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Khavaran Abbas <1953->
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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NASA Fixed Wing Project propulsion research and technology development activities to reduce thrust specific energy consumption / / Michael D. Hathaway and Ruben Del Rosario, Nateri K. Madavan
| NASA Fixed Wing Project propulsion research and technology development activities to reduce thrust specific energy consumption / / Michael D. Hathaway and Ruben Del Rosario, Nateri K. Madavan |
| Autore | Hathaway Michael D. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2013 |
| Descrizione fisica | 1 online resource (21 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Fixed wings
Energy consumption Aircraft configurations Bypass ratio Thermodynamic efficiency Thrust Hybrid propulsion Research and development |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702656603321 |
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Hathaway Michael D.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
-
Bypass ratio
(11)
- Aerodynamic noise (4)
- Noise reduction (4)
- Acoustic properties (3)
- Turbofan engines (3)