Theoretical Modelling of Aeroheating on Sharpened Noses Under Rarefied Gas Effects and Nonequilibrium Real Gas Effects

Dr. Zhi-Hui WangCurrent Affiliation: University of Chinese Academy of Sciences2002.9-2006.7 B.Sc. degree in Theoretical and Applied Mechanics, Department of Modern Mechanics, University of Science and Technology of ChinaPublication list: 1. Wang Zhihui, Bao Lin, Tong Binggang. Theoretical modeling of chemical nonequilibrium stagnation point boundary layer heat transfer under rarefied conditions. Sci China-Phys Mech Astron. 2013, 56(5):866-874.2. Wang Zhihui, Bao Lin, Tong Binggang. An analytical study on nonequilibrium dissociating gas flow behind a strong bow shockwave under rarefied conditions. Sci China-Phys Mech Astron. 2013, 56(4):671-679.3. Zhihui Wang, Lin Bao, Binggang Tong. Theoretical modeling of the chemical non-equilibrium flow behind a normal shock wave. AIAA Journal. 2012, 50(2):494-499.4. Zhihui Wang, Lin Bao, Binggang Tong. Rarefaction criterion and non-Fourier heat transfer in hypersonic rarefied flows. Physics of Fluids, 22, 126103(2010).5. Zhihui Wang, Lin Bao, Binggang Tong. Variation character of stagnation point heat flux for hypersonic pointed bodies from continuum to rarefied flow states and its bridge function study. Sci China-Phys Mech Astron. 2009, 52(12):2007-2015.6. Wang Zhihui, Bao Lin. Study on the aerothermodynamic characters of hypersonic small nose cone with local rarefied gas effects. Chinese Journal of Computational Physics, 2010, 27(1). (In Chinese)7. Wang Zhihui Bao Lin Tong Binggang, On the characteristics and physical mechanism of aeroheating to hypersonic pointed bodies with local rarefied gas effects. Physics of Gases, 2010,5(2). (In Chinese).