The development of intermittent turbulence on a swept attachment line including the effects of compressibility
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[1] K. E. Wurster. An assessment of the impact of transition on advanced winged entry vehicle thermal protection system mass , 1981 .
[2] M. R. Head,et al. The Calculation of Three-Dimensional Turbulent Boundary Layers: Part II: Attachment-Line Flow on an Infinite Swept Wing , 1967 .
[3] D. Bushnell. Interference heating on a swept cylinder in region of intersection with a wedge at Mach number 8 , 1965 .
[4] N. A. Cumpsty,et al. The Calculation of the Three-Dimensional Turbulent Boundary Layer: Part III. Comparison of Attachment-Line Calculations with Experiment , 1969 .
[5] Michael Gaster,et al. On the Flow Along Swept Leading Edges , 1965 .
[6] D. Poll,et al. Transition in the Infinite Swept Attachment Line Boundary Layer , 1979 .
[7] D. Coles,et al. Interactions for Regular Patterns of Turbulent Spots in a Laminar Boundary Layer , 1980 .
[8] N. Gregory. Transition and the Spread of Turbulence on a 60° Swept-Back Wing , 1960, The Journal of the Royal Aeronautical Society.
[9] D. Poll,et al. Skin Friction and Heat Transfer at an Infinite Swept Attachment Line , 1981 .
[10] N. A. Thyson,et al. Extension of Emmons' spot theory to flows on blunt bodies , 1971 .
[11] G. B. Schubauer,et al. Contributions on the Mechanics of Boundary-Layer Transition , 1955 .
[12] Roddam Narasimha,et al. Some properties of boundary layer flow during the transition from laminar to turbulent motion , 1958, Journal of Fluid Mechanics.
[13] I. E. Beckwith,et al. Local Heat Transfer and Recovery Temperatures on a Yawed Cylinder at a Mach Number of 4.15 and High Reynolds Numbers , 1961 .