Author:
Wang ZhiHui,Bao Lin,Tong BingGang
Publisher
Springer Science and Business Media LLC
Reference22 articles.
1. Reuther J, Kinney D, Smith S, et al. A reusable space vehicle design study exploring sharp leading edges. AIAA 2001–2884
2. Walker S P, Sullivan B J. Sharp refractory composite leading edges on hypersonic vehicles. AIAA 2003–6915
3. Fay J A, Riddell F R. Theory of stagnation point heat transfer in dissociated air. J Aeronaut Sci, 1958, 25(2): 73–85
4. Kao H C. Hypersonic viscous flow near the stagnation streamline of a blunt body: II. Third-Order Boundary-Layer theory and comparison with other methods. AIAA J, 1964, 2(11): 1898–1906
5. Paul K. Aerothermal Performance constraints for hypervelocity small radius unswept leading edges and nosetips. NASA Technical Memorandum 112204, 1997
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