Shock Standoff on Hemi-Spherical Bodies in Hypervelocity Flows

作者: F. Zander , P. A. Jacobs , R. J. Gollan , R. G. Morgan

DOI: 10.1007/978-3-319-16835-7_85

关键词:

摘要: Computational modelling of hypervelocity flows is critical in the design re-entry vehicles and validated simulation codes are required to meet this need. Bertin Cummings [1] Gnoffo et al. [2] discuss requirements importance validation computational with experimental data.

参考文章(7)
Satoshi Nonaka, Hiroyasu Mizuno, Kazuyoshi Takayama, Chul Park, Measurement of Shock Standoff Distance for Sphere in Ballistic Range Journal of Thermophysics and Heat Transfer. ,vol. 14, pp. 225- 229 ,(2000) , 10.2514/2.6512
Peter A. Gnoffo, K. James Weilmuenster, H. Harris Hamilton, David R. Olynick, Ethiraj Venkatapathy, Computational Aerothermodynamic Design Issues for Hypersonic Vehicles Journal of Spacecraft and Rockets. ,vol. 36, pp. 21- 43 ,(1999) , 10.2514/2.3430
FREDERICK S. BILLIG, Shock-wave shapes around spherical-and cylindrical-nosed bodies. Journal of Spacecraft and Rockets. ,vol. 4, pp. 822- 823 ,(1967) , 10.2514/3.28969
Stuart J. Laurence, H. G. Hornung, Image-based force and moment measurement in hypersonic facilities Experiments in Fluids. ,vol. 46, pp. 343- 353 ,(2009) , 10.1007/S00348-008-0565-6
John J. Bertin, Russell M. Cummings, Critical Hypersonic Aerothermodynamic Phenomena Annual Review of Fluid Mechanics. ,vol. 38, pp. 129- 157 ,(2006) , 10.1146/ANNUREV.FLUID.38.050304.092041