References
H. L. Reed and W. S. Saric, “Stability of three-dimensional boundary layer,” Ann. Rev. Fluid Mech,21, 235–284 (1989).
D. Arnal, Y. Casalts, and J. C. Juillen, “A survey of the transition prediction methods: from analytical criteria to PSE and DNS,” IUTAM Symp. on Laminar-Turbulent Transition. Sept 5–9, 1994. Sendai, Japan.
D. Arnal, F. Wignall, and F. Laburthe, “Recent supersonic transition studies with emphasis on the swept cylinder case,” in: Boundary Layer Transition and Control. Royal Aeronautical Society, Cambridge (1991).
T. R. Creel Jr., I. E. Beckwith, and F. J. Chen, “Transition on swept leading edge at Mach 3.5,” J. Aircr.,24, No. 10 (1987).
V. A. Lebiga, “Characteristics of pulsations in the working part of a supersonic wind tunnel,” Instability of Subsonic and Supersonic Flows. Novosibirsk (1982), pp. 123–130.
G. I. Bagaev, V. A. Lebiga, V. G. Pridanov, and V. V. Chernykh, “Supersonic wind tunnel T-325 with reduced turbulence,” in: Aerodynamic Studies. Novosibirsk (1972), pp. 11–13.
O. I. Zinin, A. D. Kosinov, N. V. Semenov, and S. G. Shevel'kov, Set of Instruments and Programs for Measuring the Nonsteady Parameters of a Supersonic Flow. Report, Institute of Theoretical and Applied Mechanics, No. 2158. Novosibirsk (1992).
B. Müller, “Experimental study of travelling waves in a three-dimensional boundary layer,” in: Laminar-Turbulent Transition Springer-Verlag, Berlin (1990), pp. 489–498.
S. A. Gaponov and A. A. Maslov, Development of Perturbations in Compressible Flows [in Russian], Nauka, Novosibirsk (1980).
Additional information
This study was conducted with financial support from the Russian Fund for Basic Research (Grant No. 94-01-000497).
Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences, 630090 Novosibirsk. Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 36, No. 6, pp. 50–54, November–December, 1995.
Rights and permissions
About this article
Cite this article
Ermolaev, Y.G., Kosinov, A.D., Levchenko, V.Y. et al. Instability of a three-dimensional supersonic boundary layer. J Appl Mech Tech Phys 36, 840–843 (1995). https://doi.org/10.1007/BF02369379
Received:
Issue Date:
DOI: https://doi.org/10.1007/BF02369379