References
- Sun MB, Zhong Z, Liang JH, et al. Experimental investigation on combustion performance of cavity-strut injection of supercritical kerosene in supersonic model combustor. Acta Astronaut. 2016;127:112–119. doi: 10.1016/j.actaastro.2016.05.035
- Narasimha R, Sreenivasan KR. Relaminarization in highly accelerated turbulent boundary layers. J Fluid Mech. 1973;61(3):417–447. doi: 10.1017/S0022112073000790
- Dussauge JP, Gaviglio J. The rapid expansion of a supersonic turbulent flow: role of bulk dilatation. J Fluid Mech. 1987;174:81–112. doi: 10.1017/S0022112087000053
- Smith DR, Smits AJ. The rapid expansion of a turbulent boundary layer in a supersonic flow. Theor Computat Fluid Dyn. 1991;2:319–328. doi: 10.1007/BF00271471
- Arnette SA, Samimy M, Elliott GS. Structure of supersonic turbulent boundary layer after expansion regions. AIAA J. 1995;33(3):430–438. doi: 10.2514/3.60007
- Arnette SA, Samimy M, Elliott GS. The effects of expansion on the turbulence structure of compressible boundary layers. J Fluid Mech. 1998;367:67–105. doi: 10.1017/S0022112098001475
- Chung KM, Lu FK. Damping of surface pressure fluctuations in hypersonic turbulent flow past expansion corners. AIAA J. 1993;31(7):1229–1234. doi: 10.2514/3.11757
- Dawson JA, Samimy M, Arnette SA. Effects of expansions on a supersonic boundary layer: surface pressure measurements. AIAA J. 1994;32(11):2169–2177. doi: 10.2514/3.12274
- Nguyen T, Behr M, Reinartz B. “Numerical investigation of compressible turbulent boundary layer over expansion corner. American Institute of Aeronautics and Astronautics. 2009. AIAA Paper 2009-7371.
- Teramoto S, Sanada H, Okamoto K. Dilatation effect in relaminarization of an accelerating supersonic turbulent boundary layer. AIAA J. 2017;55(4):1469–1474. doi: 10.2514/1.J055368
- Sun MB, Hu ZW, Sandham ND. Recovery of a supersonic turbulent boundary layer after an expansion corner. Phys Fluids. 2017;29:076103. doi: 10.1063/1.4995293
- Bookey P, Wyckham C, Smits A. New experimental data of STBLI at DNS/LES accessible Reynolds numbers, AIAA paper No. 2005-309, 2005.
- Wu M, Martin MP. Direct numerical simulation of supersonic turbulent boundary layer over a compression ramp. AIAA J. 2007;45(4):879–889. doi: 10.2514/1.27021
- Narasimha R, Viswanath PR. Reverse transition at an expansion corner in supersonic flow. AIAA J. 1975;13(5):693–695. doi: 10.2514/3.49793
- Tong FL, Li XL, Duan YH, et al. Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp. Phys Fluids. 2017;29:125101. doi: 10.1063/1.4996762
- Martin MP, Taylor EM, Wu M, et al. A bandwidth-optimized WENO scheme for the effective direct numerical simulation of compressible turbulence. J Comput Phys. 2006;220. doi: 10.1016/j.jcp.2006.05.009
- Pirozzoli S, Grasso F, Gatski TB. Direct numerical simulation and analysis of a spatially evolving supersonic turbulent boundary layer at M = 2.25. Physics of Fluids. 2004;16:530–545. doi: 10.1063/1.1637604
- Schlatter P, Orlu R. Assessment of direct numerical simulation data of turbulent boundary layers. J Fluid Mech. 2010;659:116–126. doi: 10.1017/S0022112010003113
- Pirozzoli S, Bernardini M, Grasso F. Direct numerical simulation of transonic shock/boundary layer interaction under conditions of incipient separation. J Fluid Mech. 2010;657:361–393. doi: 10.1017/S0022112010001710
- Erm LP, Joubert J. Low Reynolds number turbulent boundary layers. J Fluid Mech. 1991;230:1–44. doi: 10.1017/S0022112091000691
- Wu X, Moin P. Direct numerical simulation of turbulence in a nominally zero-pressure-gradient flat-plate boundary layer. J Fluid Mech. 2009;630:5–41. doi: 10.1017/S0022112009006624
- Hu ZW, Morfey CL, Sandham ND. Wall pressure and shear stress spectra from direct numerical simulations of channel flow up to Reτ = 1440. AIAA Journal. 2006;44(7):1541–1549. doi: 10.2514/1.17638
- Daniel CD, Laizet S, Vassilicos JC. Wall shear stress fluctuations: mixed scaling and their effects on velocity fluctuations in a turbulent boundary layer. Physics of Fluids. 2017;29:055102. doi: 10.1063/1.4984002
- Grosse S, Schröder W. Wall-shear stress patterns of coherent structures in turbulent duct flow. J Fluid Mech. 2009;633:147–158. doi: 10.1017/S0022112009007988
- Nottebrock B, Geurts KJ, Schröder W. “Wall-shear stress measurements in an adverse pressure gradient turbulent boundary layer. 2014: 2014–2098. AIAA Paper.
- Sreenivasan KR, Antonia RA. Properties of wall-shear stress fluctuations in turbulent duct flow. J Appl Mech. 1977;44:389–395. doi: 10.1115/1.3424089
- Pan C, Kwon Y. Extremely high wall-shear stress events in a turbulent boundary layer. J Phys Conf. Series. 2018;1001:012004. doi: 10.1088/1742-6596/1001/1/012004
- Bernardini M, Pirozzoli S. “Wall pressure fluctuations beneath supersonic turbulent boundary layers. Phys Fluids. 2011;23:085102. doi: 10.1063/1.3622773
- Jeong J, Hussain F. On the identification of a vortex. J Fluid Mech. 1995;285:69–94. doi: 10.1017/S0022112095000462
- Hamman CW, Klewicki JC, Kirby RW. On the Lamb vector divergence in Navier-Stokes flows. J Fluid Mech. 2008;610:261–284. doi: 10.1017/S0022112008002760
- Wietrzak A, Lueptow RM. Wall shear stress and velocity in a turbulent axisymmetric boundary layer. J Fluid Mech. 1994;259:191–218. doi: 10.1017/S0022112094000091
- Orlu R, Schlatter P. On the fluctuating wall-shear stress in zero pressure-gradient turbulent boundary layer flows. Phys Fluids. 2011;23:021704. doi: 10.1063/1.3555191
- Lenaers P, Li Q, Brethouwer G, et al. Rare backflow and extreme wall-normal velocity fluctuations in near-wall turbulence. Phys Fluids. 2012;24:035110. doi: 10.1063/1.3696304
- Jeon S, Choi H, Yoo JY, et al. Space-time characteristics of the wall shear-stress fluctuations in a low-Reynolds-number channel flow. Phys Fluids. 1999;11:3084–3094. doi: 10.1063/1.870166
- Colella KJ, Keith WL. Measurements and scaling of wall shear stress fluctuations. Exp Fluids. 2003;34:253–260. doi: 10.1007/s00348-002-0552-2