Shock-wave reflection from a turbulent boundary layer with mass bleed
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| Veröffentlicht in: | Journal of aircraft 1968-09, Vol.5 (5), p.461-467 |
|---|---|
| Hauptverfasser: | , , |
| Format: | Artikel |
| Sprache: | eng |
| Online-Zugang: | Volltext |
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| container_end_page | 467 |
|---|---|
| container_issue | 5 |
| container_start_page | 461 |
| container_title | Journal of aircraft |
| container_volume | 5 |
| creator | SEEBAUGH, WILLIAM R PAYNTER, GERALD C CHILDS, MORRIS E |
| description | |
| doi_str_mv | 10.2514/3.43967 |
| format | Article |
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| fulltext | fulltext |
| identifier | ISSN: 0021-8669 |
| ispartof | Journal of aircraft, 1968-09, Vol.5 (5), p.461-467 |
| issn | 0021-8669 1533-3868 |
| language | eng |
| recordid | cdi_aiaa_journals_10_2514_3_43967 |
| source | Alma/SFX Local Collection |
| title | Shock-wave reflection from a turbulent boundary layer with mass bleed |
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