Theoretical analysis of total pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross sectional areas:
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Washington
NACA
1958
|
| Schriftenreihe: | United States / National Advisory Committee for Aeronautics: Report
1373 |
| Beschreibung: | 26 S. Ill., graph. Darst. |
Internformat
MARC
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| 100 | 1 | |a Graves, Charles C. |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Theoretical analysis of total pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross sectional areas |c by Charles C. Graves and Jack S. Grobman |
| 246 | 1 | 3 | |a NACA TR 1373 |
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| 810 | 2 | |a National Advisory Committee for Aeronautics: Report |t United States |v 1373 |w (DE-604)BV008910189 |9 1373 | |
| 999 | |a oai:aleph.bib-bvb.de:BVB01-009139698 | ||
Datensatz im Suchindex
| _version_ | 1804128179832487936 |
|---|---|
| any_adam_object | |
| author | Graves, Charles C. Grobman, Jack S. |
| author_facet | Graves, Charles C. Grobman, Jack S. |
| author_role | aut aut |
| author_sort | Graves, Charles C. |
| author_variant | c c g cc ccg j s g js jsg |
| building | Verbundindex |
| bvnumber | BV013396621 |
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| id | DE-604.BV013396621 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T18:45:08Z |
| institution | BVB |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-009139698 |
| open_access_boolean | |
| physical | 26 S. Ill., graph. Darst. |
| publishDate | 1958 |
| publishDateSearch | 1958 |
| publishDateSort | 1958 |
| publisher | NACA |
| record_format | marc |
| series2 | United States / National Advisory Committee for Aeronautics: Report |
| spelling | Graves, Charles C. Verfasser aut Theoretical analysis of total pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross sectional areas by Charles C. Graves and Jack S. Grobman NACA TR 1373 Washington NACA 1958 26 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier United States / National Advisory Committee for Aeronautics: Report 1373 Grobman, Jack S. Verfasser aut National Advisory Committee for Aeronautics: Report United States 1373 (DE-604)BV008910189 1373 |
| spellingShingle | Graves, Charles C. Grobman, Jack S. Theoretical analysis of total pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross sectional areas |
| title | Theoretical analysis of total pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross sectional areas |
| title_alt | NACA TR 1373 |
| title_auth | Theoretical analysis of total pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross sectional areas |
| title_exact_search | Theoretical analysis of total pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross sectional areas |
| title_full | Theoretical analysis of total pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross sectional areas by Charles C. Graves and Jack S. Grobman |
| title_fullStr | Theoretical analysis of total pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross sectional areas by Charles C. Graves and Jack S. Grobman |
| title_full_unstemmed | Theoretical analysis of total pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross sectional areas by Charles C. Graves and Jack S. Grobman |
| title_short | Theoretical analysis of total pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross sectional areas |
| title_sort | theoretical analysis of total pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross sectional areas |
| volume_link | (DE-604)BV008910189 |
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