| タイトル | Performance of a High-Speed Compression-Ignition Engine Using Multiple Orifice Fuel Injection Nozzles |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930081066 |
| 著者（英） | Spanogle, J A; Foster, H H |
| 著者所属（英） | National Advisory Committee for Aeronautics. Langley Aeronautical Lab. |
| 発行日 | 1930-06-01 |
| 言語 | eng |
| 内容記述 | This report presents test results obtained at the Langley Memorial Aeronautical Laboratory of the National Advisory Committee for Aeronautics during an investigation to determine the relative performance of a single-cylinder, high-speed, compression-ignition engine when using fuel injection valve nozzles with different numbers, sizes, and directions of round orifices. A spring-loaded, automatic injection valve was used, centrally located at the top of a vertical disk-type combustion chamber formed between horizontally opposed inlet and exhaust valves of a 5 inch by 7 inch engine. |
| レポートNO | 93R10356
NACA-TN-344 |
| 権利 | No Copyright |
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