Variation character of stagnation point heat flux for hypersonic pointed bodies from continuum to rarefied flow states and its bridge function study

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

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