Author:
Wu Song,Shu Yong-Hua,Li Jin-Ping,Yu Hong-Ru
Publisher
Springer Science and Business Media LLC
Reference10 articles.
1. Nakakita K, Osafune T, Asai K. Global heat transfer measurement in a hypersonic shock tunnel using temperature-sensitive. AIAA-2003-0743
2. Hubner J, Carroll B, Schanze K et al. Temperature and pressure sensitive paint measurements in short duration hypersonic flow. AIAA-99-0388
3. Oliver H. Thin-film gauges and coaxial thermocouples for measuring transient temperatures. (Description-gauges2.pdf, from http://www.swl.rwth-aachen.de )
4. Holden MS. A database of aerothermal measurements in hypersonic flow in building block experiments for CFD validation. AIAA Paper 2003-1137
5. Zhang SZ, Chen H, Dong ZC et al (2010) Heat flux measurement at stagnation point in high-enthalpy shock tubes. In: Proceedings of the 14th Chinese National Symposium on Shock Waves (in Chinese)
Cited by
4 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献