Boundary-Layer Transition on Cones Near Mach One
Review of some data which demonstrate the possibility of using an aeroballistic range for obtaining transition Reynolds numbers near a Mach number of one. The results obtained are believed to offer adequate proof of the feasibility of interference-free data for free-stream Mach numbers greater than...
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Veröffentlicht in: | AIAA journal 1974-04, Vol.12 (4), p.570-571 |
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Format: | Artikel |
Sprache: | eng |
Online-Zugang: | Volltext |
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Zusammenfassung: | Review of some data which demonstrate the possibility of using an aeroballistic range for obtaining transition Reynolds numbers near a Mach number of one. The results obtained are believed to offer adequate proof of the feasibility of interference-free data for free-stream Mach numbers greater than 1.04, using 6.4-cm-diam 10-deg semiangle sharp cones in a 1.8-m-diam aeroballistic range. |
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ISSN: | 0001-1452 1533-385X |
DOI: | 10.2514/3.49293 |