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Stability Theory as a Guide to the Evaluation of Transition Data
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Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer Transition
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Direct Numerical Simulation of Laminar Breakdown in High-Speed, Axisymmetric Boundary Layers
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On the Structure of Hypersonic Turbulent Boundary Layers
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On the Structure of High-Reynolds-Number Supersonic Turbulent Boundary Layers
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Hypersonic Transitional Boundary Layers
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Mack, L. M., "Boundary-Layer Stability Analysis for Sharp Cones at Zero Angle-of-Attack," U.S. Air Force Wright Aeronautical Lab., Rept. AFWAL-TR-86-3022, Wright-Patterson AFB, OH, Aug. 1986.
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Characteristics of Hot Film Anemometers for Use in Hypersonic Flows
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0027238977
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Experimental Transition Zone Lengths in Pressure Gradient in Hypersonic Flow
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Kimmel, R. L., "Experimental Transition Zone Lengths in Pressure Gradient in Hypersonic Flow," Transitional and Turbulent Compressible Flows, edited by L. D. Krai and T. A. Zang, ASME FED-Vol. 151, American Society of Mechanical Engineers, New York, 1993, pp. 117-128.
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