The calculation of pressure on slender airplanes in subsonic and supersonic flow
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Washington
NACA
1954
|
| Schriftenreihe: | United States / National Advisory Committee for Aeronautics: Report
1185 |
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| 100 | 1 | |a Heaslet, Max A. |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a The calculation of pressure on slender airplanes in subsonic and supersonic flow |c by Max A. Heaslet and Harvard Lomax |
| 246 | 1 | 3 | |a NACA TR 1185 |
| 264 | 1 | |a Washington |b NACA |c 1954 | |
| 300 | |a 11 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 1185 | |
| 700 | 1 | |a Lomax, Harvard |d 1922-1999 |e Verfasser |0 (DE-588)13051604X |4 aut | |
| 810 | 2 | |a National Advisory Committee for Aeronautics: Report |t United States |v 1185 |w (DE-604)BV008910189 |9 1185 | |
| 943 | 1 | |a oai:aleph.bib-bvb.de:BVB01-009024501 | |
Datensatz im Suchindex
| _version_ | 1819245232453058560 |
|---|---|
| any_adam_object | |
| author | Heaslet, Max A. Lomax, Harvard 1922-1999 |
| author_GND | (DE-588)13051604X |
| author_facet | Heaslet, Max A. Lomax, Harvard 1922-1999 |
| author_role | aut aut |
| author_sort | Heaslet, Max A. |
| author_variant | m a h ma mah h l hl |
| building | Verbundindex |
| bvnumber | BV013242061 |
| ctrlnum | (DE-599)BVBBV013242061 |
| format | Book |
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| id | DE-604.BV013242061 |
| illustrated | Illustrated |
| indexdate | 2024-12-23T15:24:13Z |
| institution | BVB |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-009024501 |
| open_access_boolean | |
| physical | 11 S. Ill., graph. Darst. |
| publishDate | 1954 |
| publishDateSearch | 1954 |
| publishDateSort | 1954 |
| publisher | NACA |
| record_format | marc |
| series2 | United States / National Advisory Committee for Aeronautics: Report |
| spelling | Heaslet, Max A. Verfasser aut The calculation of pressure on slender airplanes in subsonic and supersonic flow by Max A. Heaslet and Harvard Lomax NACA TR 1185 Washington NACA 1954 11 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier United States / National Advisory Committee for Aeronautics: Report 1185 Lomax, Harvard 1922-1999 Verfasser (DE-588)13051604X aut National Advisory Committee for Aeronautics: Report United States 1185 (DE-604)BV008910189 1185 |
| spellingShingle | Heaslet, Max A. Lomax, Harvard 1922-1999 The calculation of pressure on slender airplanes in subsonic and supersonic flow |
| title | The calculation of pressure on slender airplanes in subsonic and supersonic flow |
| title_alt | NACA TR 1185 |
| title_auth | The calculation of pressure on slender airplanes in subsonic and supersonic flow |
| title_exact_search | The calculation of pressure on slender airplanes in subsonic and supersonic flow |
| title_full | The calculation of pressure on slender airplanes in subsonic and supersonic flow by Max A. Heaslet and Harvard Lomax |
| title_fullStr | The calculation of pressure on slender airplanes in subsonic and supersonic flow by Max A. Heaslet and Harvard Lomax |
| title_full_unstemmed | The calculation of pressure on slender airplanes in subsonic and supersonic flow by Max A. Heaslet and Harvard Lomax |
| title_short | The calculation of pressure on slender airplanes in subsonic and supersonic flow |
| title_sort | the calculation of pressure on slender airplanes in subsonic and supersonic flow |
| volume_link | (DE-604)BV008910189 |
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