Ballistic Range Experiment of Shock Stand-Off Distance for Spheres in Air with Flight Speeds Between 5.08 and 6.49 km/s

Author:

Dongjun Liao,Liu Sen,Jian Hexiang,Aimin Xie,Wang Zonghao,Huang Jie

Publisher

Springer International Publishing

Reference21 articles.

1. Liao, D., Liu, S., Jian, H., et al.: Review of research on shock standoff distance for hypersonic sphere. J. Exp. Fuid Mech. 29(6), 1–7 (2015)

2. Park, C.: The limits of two-temperature model. AIAA. 911 (2010)

3. Spurk, J.H.: Experimental and numerical nonequilibrium studies. AIAA J. 8(6), 1039–1045 (1970)

4. Hornung, H.G.: Non-equilibrium dissociating nitrogen flow over spheres and circular cylinders. J. Fluid Mech. 64(4), 725–736 (1974)

5. Miller III, C.G.: Shock shapes on blunt bodies in hypersonic-hypervelocity helium, air, and $$CO_2$$ flows, and calibration results in Langley 6-inch expansion tube. NASA TN D-7800 (1975)

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