“…Thermoelastohydrodynamic problems have always played an essential role in the precise design of gas face seals [ 1 , 2 , 3 , 4 , 5 , 6 ] and other mechanical elements [ 7 , 8 , 9 , 10 ] since both thermal distortion and elastic distortion significantly affect sealing performance. However, with the rapid development of pre-cool technology using low-temperature and high-pressure helium gas in hypersonic engines [ 11 , 12 ], there arouses a new thermoelastohydrodynamic lubrication problem, where not only the face distortions [ 13 , 14 , 15 , 16 ] but also the real-gas properties [ 17 , 18 ] become nonignorable, since compressibility coefficient, viscosity, and heat capacity vary obviously with decreasing temperature.…”