Boundary-Layer Transition on Cones Near Mach One

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
1. Verfasser: POTTER, J. LEITH
Format: Artikel
Sprache:eng
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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.
ISSN:0001-1452
1533-385X
DOI:10.2514/3.49293