Some effects of injection advance angle, engine jacket temperature, and speed on combustion in a compression ignition engine:
Gespeichert in:
| Beteiligte Personen: | , |
|---|---|
| Format: | Buch |
| Sprache: | Englisch |
| Veröffentlicht: |
Washington
NACA
1935
|
| Schriftenreihe: | United States / National Advisory Committee for Aeronautics: Report
525 |
| Umfang: | 15 S. Ill., graph. Darst. |
Internformat
MARC
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| 100 | 1 | |a Rothrock, Addison M. |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Some effects of injection advance angle, engine jacket temperature, and speed on combustion in a compression ignition engine |c by A. M. Rothrock and C. D. Waldron |
| 246 | 1 | 3 | |a NACA TR 525 |
| 246 | 1 | 3 | |a Some effects of injection advance angle, engine-jacket temperature, and speed on combustion in a compression-ignition engine |
| 264 | 1 | |a Washington |b NACA |c 1935 | |
| 300 | |a 15 S. |b Ill., graph. Darst. | ||
| 336 | |b txt |2 rdacontent | ||
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| 490 | 1 | |a United States / National Advisory Committee for Aeronautics: Report |v 525 | |
| 700 | 1 | |a Waldron, C. D. |e Verfasser |4 aut | |
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Datensatz im Suchindex
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| any_adam_object | |
| author | Rothrock, Addison M. Waldron, C. D. |
| author_facet | Rothrock, Addison M. Waldron, C. D. |
| author_role | aut aut |
| author_sort | Rothrock, Addison M. |
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| building | Verbundindex |
| bvnumber | BV013174654 |
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| id | DE-604.BV013174654 |
| illustrated | Illustrated |
| indexdate | 2024-12-20T10:42:28Z |
| institution | BVB |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-008976164 |
| open_access_boolean | |
| physical | 15 S. Ill., graph. Darst. |
| publishDate | 1935 |
| publishDateSearch | 1935 |
| publishDateSort | 1935 |
| publisher | NACA |
| record_format | marc |
| series2 | United States / National Advisory Committee for Aeronautics: Report |
| spelling | Rothrock, Addison M. Verfasser aut Some effects of injection advance angle, engine jacket temperature, and speed on combustion in a compression ignition engine by A. M. Rothrock and C. D. Waldron NACA TR 525 Some effects of injection advance angle, engine-jacket temperature, and speed on combustion in a compression-ignition engine Washington NACA 1935 15 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier United States / National Advisory Committee for Aeronautics: Report 525 Waldron, C. D. Verfasser aut National Advisory Committee for Aeronautics: Report United States 525 (DE-604)BV008910189 525 |
| spellingShingle | Rothrock, Addison M. Waldron, C. D. Some effects of injection advance angle, engine jacket temperature, and speed on combustion in a compression ignition engine |
| title | Some effects of injection advance angle, engine jacket temperature, and speed on combustion in a compression ignition engine |
| title_alt | NACA TR 525 Some effects of injection advance angle, engine-jacket temperature, and speed on combustion in a compression-ignition engine |
| title_auth | Some effects of injection advance angle, engine jacket temperature, and speed on combustion in a compression ignition engine |
| title_exact_search | Some effects of injection advance angle, engine jacket temperature, and speed on combustion in a compression ignition engine |
| title_full | Some effects of injection advance angle, engine jacket temperature, and speed on combustion in a compression ignition engine by A. M. Rothrock and C. D. Waldron |
| title_fullStr | Some effects of injection advance angle, engine jacket temperature, and speed on combustion in a compression ignition engine by A. M. Rothrock and C. D. Waldron |
| title_full_unstemmed | Some effects of injection advance angle, engine jacket temperature, and speed on combustion in a compression ignition engine by A. M. Rothrock and C. D. Waldron |
| title_short | Some effects of injection advance angle, engine jacket temperature, and speed on combustion in a compression ignition engine |
| title_sort | some effects of injection advance angle engine jacket temperature and speed on combustion in a compression ignition engine |
| volume_link | (DE-604)BV008910189 |
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