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Design and cold-air investigation of a turbine for a small low-cost turbofan engine / / by Milton G. Kofskey and William J. Nusbaum
| Design and cold-air investigation of a turbine for a small low-cost turbofan engine / / by Milton G. Kofskey and William J. Nusbaum |
| Autore | Kofskey Milton G. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , September 1972 |
| Descrizione fisica | 1 online resource (31 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Gas turbines
Axial flow Airplanes - Turbofan engines Axial flow compressors Low temperatures Gas-turbines - Testing |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716571503321 |
Kofskey Milton G.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , September 1972 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Effects of tip clearance on overall performance of transonic fan stage with and without casing treatment / / Royce D. Moore and Walter M. Osborn
| Effects of tip clearance on overall performance of transonic fan stage with and without casing treatment / / Royce D. Moore and Walter M. Osborn |
| Autore | Moore Royce D. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , February 1977 |
| Descrizione fisica | 1 online resource (approximately 27 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Casing
Turbofan engines Transonic flow Aerodynamics, Transonic Airplanes - Turbofan engines Airplanes - Turbojet engines - Blades Compressors - Aerodynamics Compressors - Blades |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717186303321 |
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Moore Royce D.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , February 1977 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Rate-based model predictive control of turbofan engine clearance [[electronic resource] /] / Jonathan A. DeCastro
| Rate-based model predictive control of turbofan engine clearance [[electronic resource] /] / Jonathan A. DeCastro |
| Autore | DeCastro Jonathan A |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2006] |
| Descrizione fisica | 1 online resource (14 pages) : illustrations |
| Collana | NASA/CR |
| Soggetto topico | Airplanes - Turbofan engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697245903321 |
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DeCastro Jonathan A
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2006] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Static performance of six innovative thrust reverser concepts for subsonic transport applications : summary of the NASA Langley Innovative Thrust Reverser Test Program / / Scott C. Asbury and Jeffrey A. Yetter
| Static performance of six innovative thrust reverser concepts for subsonic transport applications : summary of the NASA Langley Innovative Thrust Reverser Test Program / / Scott C. Asbury and Jeffrey A. Yetter |
| Autore | Asbury Scott C. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 2000 |
| Descrizione fisica | 1 online resource (30 pages, 334 unnumbered pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Airplanes - Brakes
Airplanes - Design and construction Airplanes - Motors - Thrust Airplanes - Turbofan engines Jet planes - Thrust reversers - Testing Thrust reversal Turbofans Aeronautical engineering Aircraft design Performance tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Static performance of six innovative thrust reverser concepts for subsonic transport applications |
| Record Nr. | UNINA-9910707886903321 |
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Asbury Scott C.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 2000 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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STOVL propulsion system volume dynamics approximations [[electronic resource] /] / Colin K. Drummond
| STOVL propulsion system volume dynamics approximations [[electronic resource] /] / Colin K. Drummond |
| Autore | Drummond Colin K |
| Pubbl/distr/stampa | Cleveland, Ohio : , : NASA, Lewis Research Center, , [1989] |
| Descrizione fisica | 1 online resource (9 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Computerized simulation
Propulsion system configurations Short takeoff aircraft Turbofan engines Vertical landing Computer simulation Propulsion systems Airplanes - Turbofan engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701452803321 |
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Drummond Colin K
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| Cleveland, Ohio : , : NASA, Lewis Research Center, , [1989] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Type certification basis for conversion from reciprocating engine to turbine engine-powered part 23 airplanes [[electronic resource]]
| Type certification basis for conversion from reciprocating engine to turbine engine-powered part 23 airplanes [[electronic resource]] |
| Pubbl/distr/stampa | [Washington, D.C.] : , : U.S. Dept. of Transportation, Federal Aviation Administration, , [1993] |
| Descrizione fisica | 6, 2 pages : digital, PDF file |
| Collana | Advisory circular |
| Soggetto topico |
Airplanes, Military - Turbofan engines
Airplanes - Turbofan engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697739603321 |
| [Washington, D.C.] : , : U.S. Dept. of Transportation, Federal Aviation Administration, , [1993] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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