Info
Effect of shortening transition liner to decrease overall length of a ram induction combustor / / by Donald F. Schultz, Porter J. Perkins, and Jerrold D. Wear
| Effect of shortening transition liner to decrease overall length of a ram induction combustor / / by Donald F. Schultz, Porter J. Perkins, and Jerrold D. Wear |
| Autore | Schultz Donald F. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , December 1970 |
| Descrizione fisica | 1 online resource (18 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Turbojet engines
Combustion chambers Airplanes - Turbojet engines - Combustion Smoke Combustion - Research Combustion chambers - Testing |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716552303321 |
Schultz Donald F.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , December 1970 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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High-pressure combustor exhaust emissions with improved air-atomizing and conventional pressure-atomizing fuel nozzles / / by Robert D. Ingebo and Carl T. Norgren
| High-pressure combustor exhaust emissions with improved air-atomizing and conventional pressure-atomizing fuel nozzles / / by Robert D. Ingebo and Carl T. Norgren |
| Autore | Ingebo Robert D. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , February 1973 |
| Descrizione fisica | 1 online resource (22 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Combustion chambers
Spray nozzles Aircraft exhaust emissions Airplanes - Turbojet engines - Combustion Combustion chambers - Testing Spray nozzles - Testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716670603321 |
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Ingebo Robert D.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , February 1973 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Performance of a high-speed compression-ignition engine using multiple orifice fuel injection nozzles / / by J.A. Spanogle and H.H. Foster
| Performance of a high-speed compression-ignition engine using multiple orifice fuel injection nozzles / / by J.A. Spanogle and H.H. Foster |
| Autore | Spanogle J. A. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1930 |
| Descrizione fisica | 1 online resource (18 pages, 21 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Motors - Fuel injection systems - Testing
Combustion chambers - Testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910714049603321 |
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Spanogle J. A.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1930 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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