Theoretical and experimental analysis of low drag supersonic inlets having a circular cross section and a central body at mach numbers of 3.30, 2.75 , and 2.45:
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Washington
NACA
1954
|
| Schriftenreihe: | United States / National Advisory Committee for Aeronautics: Report
1189 |
| Beschreibung: | 37 S. Ill., graph. Darst. |
Internformat
MARC
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| 100 | 1 | |a Ferri, Antonio |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Theoretical and experimental analysis of low drag supersonic inlets having a circular cross section and a central body at mach numbers of 3.30, 2.75 , and 2.45 |c by Antonio Ferri and Louis M. Nucci |
| 246 | 1 | 3 | |a NACA TR 1189 |
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Datensatz im Suchindex
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| author | Ferri, Antonio Nucci, Louis M. |
| author_facet | Ferri, Antonio Nucci, Louis M. |
| author_role | aut aut |
| author_sort | Ferri, Antonio |
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| id | DE-604.BV013242242 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T18:42:19Z |
| institution | BVB |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-009024660 |
| open_access_boolean | |
| physical | 37 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 | Ferri, Antonio Verfasser aut Theoretical and experimental analysis of low drag supersonic inlets having a circular cross section and a central body at mach numbers of 3.30, 2.75 , and 2.45 by Antonio Ferri and Louis M. Nucci NACA TR 1189 Washington NACA 1954 37 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier United States / National Advisory Committee for Aeronautics: Report 1189 Nucci, Louis M. Verfasser aut National Advisory Committee for Aeronautics: Report United States 1189 (DE-604)BV008910189 1189 |
| spellingShingle | Ferri, Antonio Nucci, Louis M. Theoretical and experimental analysis of low drag supersonic inlets having a circular cross section and a central body at mach numbers of 3.30, 2.75 , and 2.45 |
| title | Theoretical and experimental analysis of low drag supersonic inlets having a circular cross section and a central body at mach numbers of 3.30, 2.75 , and 2.45 |
| title_alt | NACA TR 1189 |
| title_auth | Theoretical and experimental analysis of low drag supersonic inlets having a circular cross section and a central body at mach numbers of 3.30, 2.75 , and 2.45 |
| title_exact_search | Theoretical and experimental analysis of low drag supersonic inlets having a circular cross section and a central body at mach numbers of 3.30, 2.75 , and 2.45 |
| title_full | Theoretical and experimental analysis of low drag supersonic inlets having a circular cross section and a central body at mach numbers of 3.30, 2.75 , and 2.45 by Antonio Ferri and Louis M. Nucci |
| title_fullStr | Theoretical and experimental analysis of low drag supersonic inlets having a circular cross section and a central body at mach numbers of 3.30, 2.75 , and 2.45 by Antonio Ferri and Louis M. Nucci |
| title_full_unstemmed | Theoretical and experimental analysis of low drag supersonic inlets having a circular cross section and a central body at mach numbers of 3.30, 2.75 , and 2.45 by Antonio Ferri and Louis M. Nucci |
| title_short | Theoretical and experimental analysis of low drag supersonic inlets having a circular cross section and a central body at mach numbers of 3.30, 2.75 , and 2.45 |
| title_sort | theoretical and experimental analysis of low drag supersonic inlets having a circular cross section and a central body at mach numbers of 3 30 2 75 and 2 45 |
| volume_link | (DE-604)BV008910189 |
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