Experimental investigation of transonic and supersonic flow over a sphere for Reynolds numbers of 103–105 by free-flight tests with schlieren visualization.
| Autor: | Nagata, T.1 nagata.takayuki@aero.mech.tohoku.ac.jp, Noguchi, A.1, Nonomura, T.1, Ohtani, K.2, Asai, K.1 |
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| Zdroj: | Shock Waves. Mar2020, Vol. 30 Issue 2, p139-151. 13p. |
| Databáze: | Academic Search Ultimate |
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