No data available.
Please log in to see this content.
You have no subscription access to this content.
No metrics data to plot.
The attempt to load metrics for this article has failed.
The attempt to plot a graph for these metrics has failed.
The full text of this article is not currently available.
Transition in hypersonic boundary layers
6.L. M. Mack, Boundary-layer stability theory (Jet Propulsion Laboratory, Pasadena, CA, 1969), Doc. 900-277.
7.M. R. Malik, in Laminar Turbulent Boundary Layers; Proceedings of the Energy Sources Technology Conferences, edited by E. M. Uram and H. E. Weber (ASME, 1984), pp. 139–147.
8.G. Gasperas, AIAA Paper 1987-0494 (1987).
9.L. M. Mack, AIAA Paper 1987-1413 (1987).
10.S. P. Wilkinson, AIAA Paper 1997-1819 (1997).
11.J. W. Hofferth and W. S. Saric, AIAA Paper 2012-0923 (2012).
12.S. P. Schneider, AIAA Paper 2013-2608 (2013).
18.A. C. Laible and H. F. Fasel, AIAA Paper 2011-3565 (2011).
22.D. A. Bountin, A. N. Shiplyuk, and A. A. Sidorenko, in Laminar-Turbulent Transition, edited by H. F. Fasel and W. S. Saric (Springer, 2000), pp. 475–480.
25.S. P. Schneidery, AIAA Paper 2007-0305 (2007).
26.P. S. Iyer, S. Muppidi, and K. Mahesh, AIAA Paper 2011-566 (2011).
32.C. S. Moraitis and M. L. Riethmuller, in 4th International Symposium on Application of Laser Anemometry to Fluid Dynamics (Lisbon, Portugal, 1988).
33.F. Scarano, in Advanced Measurement Techniques for Supersonic Flows, edited by M. L. Riethmuller and F. Scarano (von Karman Institute, Belgium, 2005).
34.C. H. Zhang, “The development of hypersonic quiet wind tunnel and experimental investigation of hypersonic boundary-layer transition on a flared cone,” Ph.D. thesis, Peking University (2014).
35.C. R. Alba, K. M. Casper, S. J. Beresh, and S. P. Schneider, AIAA Paper 2010-0897 (2010).
Article metrics loading...
Transition and turbulence production in a hypersonic boundary layer is investigated in a Mach 6 wind tunnel using Rayleigh-scattering visualization, fast-response pressure measurements, and particle image
velocimetry. It is found that the second-mode instability is a key modulator of the transition process. Although the second-mode is primarily an acoustic wave, it causes the formation of high-frequency vortical waves, which triggers a fast transition to turbulence.
Full text loading...
Most read this month