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2010 Fifth International Conference on Frontier of Computer Science and Technology
Numerical Simulation on Aerodynamic Heating Process and Research on the Missile Head Structure
Changchun, Jilin Province, China
August 18-August 22
ISBN: 978-0-7695-4139-6
| ASCII Text | x | ||
| Bowei Liu, Yanli Ma, Yi Jiang, Weichen Wang, Yongyuan Li, Liwu Shao, "Numerical Simulation on Aerodynamic Heating Process and Research on the Missile Head Structure," 2010 Fifth International Conference on Frontier of Computer Science and Technology, pp. 184-186, 2010 Fifth International Conference on Frontier of Computer Science and Technology, 2010. | |||
| BibTex | x | ||
| @article{ 10.1109/FCST.2010.47, author = {Bowei Liu and Yanli Ma and Yi Jiang and Weichen Wang and Yongyuan Li and Liwu Shao}, title = {Numerical Simulation on Aerodynamic Heating Process and Research on the Missile Head Structure}, journal ={2010 Fifth International Conference on Frontier of Computer Science and Technology}, volume = {0}, year = {2010}, isbn = {978-0-7695-4139-6}, pages = {184-186}, doi = {http://doi.ieeecomputersociety.org/10.1109/FCST.2010.47}, publisher = {IEEE Computer Society}, address = {Los Alamitos, CA, USA}, } | |||
| RefWorks Procite/RefMan/Endnote | x | ||
| TY - CONF JO - 2010 Fifth International Conference on Frontier of Computer Science and Technology TI - Numerical Simulation on Aerodynamic Heating Process and Research on the Missile Head Structure SN - 978-0-7695-4139-6 SP184 EP186 A1 - Bowei Liu, A1 - Yanli Ma, A1 - Yi Jiang, A1 - Weichen Wang, A1 - Yongyuan Li, A1 - Liwu Shao, PY - 2010 KW - aerodynamic heating KW - fluid-solid coupled KW - numerical simulation KW - ballistic trajectory KW - shock wave VL - 0 JA - 2010 Fifth International Conference on Frontier of Computer Science and Technology ER - | |||
DOI Bookmark: http://doi.ieeecomputersociety.org/10.1109/FCST.2010.47
In order to calculate the aerodynamic heating process of the missile head, the environmental temperature and pressure are obtained by the ballistic trajectory table and the flight Mach number are calculated. The method of fluid-solid coupled was used to compute the inner and outer field of the missile. The temperature of the missile surface and head was obtained. The result shows the fluid-solid coupled method is suitable for the aerodynamic heating calculation. The inflexion of the missile should be considered respectively at the subsonic and the supersonic flight in the design of the missile.
Index Terms:
aerodynamic heating, fluid-solid coupled, numerical simulation, ballistic trajectory, shock wave
Citation:
Bowei Liu, Yanli Ma, Yi Jiang, Weichen Wang, Yongyuan Li, Liwu Shao, "Numerical Simulation on Aerodynamic Heating Process and Research on the Missile Head Structure," fcst, pp.184-186, 2010 Fifth International Conference on Frontier of Computer Science and Technology, 2010
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