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NACA-TR-1356
Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition
Year: 1958
Abstract: Report presents the results of experimental and theoretical research conducted on flow separation associated with steps, bases, compression corners, curved surfaces, shock-wave boundary-layer reflections, and configurations producing leading-edge separation. Results were obtained from pressure-distribution measurements, shadowgraph observations, high-speed motion pictures, and oil-film studies. The maximum scope of measurement encompassed Mach numbers between 0.4 and 3.6, and length Reynolds numbers between 4,000 and 5,000,000.
Subject: BOUNDARY
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:09:09Z | |
| date available | 2017-09-04T18:09:09Z | |
| date copyright | 01/01/1958 | |
| date issued | 1958 | |
| identifier other | GTUYYDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/192209 | |
| description abstract | Report presents the results of experimental and theoretical research conducted on flow separation associated with steps, bases, compression corners, curved surfaces, shock-wave boundary-layer reflections, and configurations producing leading-edge separation. Results were obtained from pressure-distribution measurements, shadowgraph observations, high-speed motion pictures, and oil-film studies. The maximum scope of measurement encompassed Mach numbers between 0.4 and 3.6, and length Reynolds numbers between 4,000 and 5,000,000. | |
| language | English | |
| title | NACA-TR-1356 | num |
| title | Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition | en |
| type | standard | |
| page | 40 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1958 | |
| contenttype | fulltext | |
| subject keywords | BOUNDARY | |
| subject keywords | CROCCO | |
| subject keywords | DIMENSIONAL | |
| subject keywords | FLAT | |
| subject keywords | FLOW | |
| subject keywords | LAMINAR | |
| subject keywords | LAYER | |
| subject keywords | LEE | |
| subject keywords | MACH | |
| subject keywords | NUMBER | |
| subject keywords | PLATES | |
| subject keywords | POINTS | |
| subject keywords | REATTACHED | |
| subject keywords | REYNOLDS | |
| subject keywords | SEPARATED | |
| subject keywords | SEPARATION | |
| subject keywords | SUBSONIC | |
| subject keywords | SUPERSONIC | |
| subject keywords | TESTS | |
| subject keywords | THEORY | |
| subject keywords | TRANSITION | |
| subject keywords | TUNNEL | |
| subject keywords | TURBULENT | |
| subject keywords | TWO | |
| subject keywords | WIND |