Three-dimensional transonic flow theory applied to slender wings and bodies:
Saved in:
| Main Authors: | , |
|---|---|
| Format: | Book |
| Language: | English |
| Published: |
Washington
NACA
1957
|
| Series: | United States / National Advisory Committee for Aeronautics: Report
1318 |
| Physical Description: | 29 S. Ill., graph. Darst. |
Staff View
MARC
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Record in the Search Index
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|---|---|
| any_adam_object | |
| author | Heaslet, Max. A. Spreiter, John R. |
| author_facet | Heaslet, Max. A. Spreiter, John R. |
| author_role | aut aut |
| author_sort | Heaslet, Max. A. |
| author_variant | m a h ma mah j r s jr jrs |
| building | Verbundindex |
| bvnumber | BV013253739 |
| ctrlnum | (DE-599)BVBBV013253739 |
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| id | DE-604.BV013253739 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T18:42:33Z |
| institution | BVB |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-009033895 |
| open_access_boolean | |
| physical | 29 S. Ill., graph. Darst. |
| publishDate | 1957 |
| publishDateSearch | 1957 |
| publishDateSort | 1957 |
| publisher | NACA |
| record_format | marc |
| series2 | United States / National Advisory Committee for Aeronautics: Report |
| spelling | Heaslet, Max. A. Verfasser aut Three-dimensional transonic flow theory applied to slender wings and bodies by Max. A. Heaslet and John R. Spreiter NACA TR 1318 Washington NACA 1957 29 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier United States / National Advisory Committee for Aeronautics: Report 1318 Spreiter, John R. Verfasser aut National Advisory Committee for Aeronautics: Report United States 1318 (DE-604)BV008910189 1318 |
| spellingShingle | Heaslet, Max. A. Spreiter, John R. Three-dimensional transonic flow theory applied to slender wings and bodies |
| title | Three-dimensional transonic flow theory applied to slender wings and bodies |
| title_alt | NACA TR 1318 |
| title_auth | Three-dimensional transonic flow theory applied to slender wings and bodies |
| title_exact_search | Three-dimensional transonic flow theory applied to slender wings and bodies |
| title_full | Three-dimensional transonic flow theory applied to slender wings and bodies by Max. A. Heaslet and John R. Spreiter |
| title_fullStr | Three-dimensional transonic flow theory applied to slender wings and bodies by Max. A. Heaslet and John R. Spreiter |
| title_full_unstemmed | Three-dimensional transonic flow theory applied to slender wings and bodies by Max. A. Heaslet and John R. Spreiter |
| title_short | Three-dimensional transonic flow theory applied to slender wings and bodies |
| title_sort | three dimensional transonic flow theory applied to slender wings and bodies |
| volume_link | (DE-604)BV008910189 |
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