Publisher
Springer Berlin Heidelberg
Reference10 articles.
1. Holden, M.S.: Boundary-layer displacement and leading-edge bluntness effects on attached and separated laminar boundary layers in a compression corner. Part II: Experimental study., AIAA Journal Vol. 9, No. 1 (1971) pp. 84-93.
2. Mallinson, S.G., Gai, S.L., Mudford, N.R.: Leading-edge bluntness effects in high enthalpy, hypersonic compression corner flow, AIAA Journal Vol. 34, No. 11 (1996) pp. 2284-2290
3. Reinartz, B., Ballmann, J.: Numerical simulation of wall temperature and entropy layer effects on double wedge shock/boundary layer interactions, AIAA Paper 2006-8137, 14th AIAA/AHI Space Planes Conference and Hypersonic Systems Conference, Canberra, Australia (2006)
4. Neuenhahn, T., Olivier, H.: Influence of the wall temperature and the entropy layer effects on double wedge shock boundary layer interactions., AIAA Paper 2006-8136, 14th AIAA/AHI Space Planes Conference and Hypersonic Systems Conference, Canberra, Australia (2006)
5. Cheng, H.K. et al.: Boundary layer displacement and leading-edge bluntness effects in high-temperature hypersonic flow, Journal of Aerospace Science Vol. 28, No. 5 (1961) pp. 353-381
Cited by
5 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