Direct numerical simulation of hypersonic turbulent boundary layers. Part 2. Effect of wall temperature

By Lian Duan, I. Beekman, M. Pino Martín. Journal of Fluid Mechanics, 2010

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A generalized Reynolds analogy for compressible wall-bounded turbulent flows (2013, methodology): “Some studies have used Tw/Tδ or Tw/Tf (where Tf is a reference temperature) to define the dimensionless wall temperature (Duan et al. 2010).”
Physics and Measurement of Aero-Optical Effects: Past and Present (2017, background): “…of the aero-optical distortions, numerous experimental (Spina et al. 1994, Smits & Dussauge 1996) and numerical (Gaviglio 1987, Guarini et al. 2000, Duan et al. 2010, Wang & Wang 2013) studies in boundary layers have shown that the time-averaged pressure fluctuations are several times smaller than…”
Turbulence in supersonic boundary layers at moderate Reynolds number (2011, background): “The validity of Morkovin’s density scaling has been addressed in a series of recent studies (Duan et al. 2010, 2011; Lagha et al. 2011), which indicate moderate success in scaling mean and fluctuating velocity distributions across a range of Mach numbers, also in the presence of heated and cooled…”