Laminar Base Flow Downstream of Slender Cones in Hypersonic Flow

1. P.K. Chang, Separation of Flows, Pergamon, Oxford (1970).

   Google Scholar 

2. A. I. Shvetz and I. T. Shvetz, Gas Dynamics of the Near Wake [in Russian], Naukova Dumka, Kiev (1976).

   Google Scholar 

3. L.V. Gogish and G.Yu. Stepanov, Separation and Cavitation Flows [in Russian], Nauka, Moscow (1990).

   Google Scholar 

4. D. R. Chapman, “An analysis of base pressure at supersonic velocities and comparison with experiment,” NACA Techn. Note, No. 2137 (1950).

5. H.H. Korst, “A theory for base pressures in transonic and supersonic flows,” J. Appl. Mech., 23, 593 (1956).

   Google Scholar 

6. N. S. Matveeva and N. S. Neyland, “The laminar boundary layer near a body corner point,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 4, 64 (1967).

   Google Scholar 

7. V.Ya. Neyland, “Asymptotic theory for calculating heat fluxes near the corner of a body,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 5, 53 (1969).

   Google Scholar 

8. V.Ya. Neyland, “Peculiarities of the boundary layer separation on a cooled body and its interaction with a hypersonic flow,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 6, 99 (1973).

   Google Scholar 

9. V. M. Kovenya and A. S. Lebedev, “Numerical simulation of viscous separated near-wake flows,” Zh. Prikl. Mekh. Tekhn. Fiz., No. 5, 53 (1989).

   Google Scholar 

10. F. Grasso and C. Pettinelli, “Analysis of laminar near-wake hypersonic flows,” J. Spacecr. Rock., 32, 970 (1995).

    Google Scholar 

11. J. P. Lamb and W. L. Oberkampf, “Review and development of base pressure and base heating correlations in supersonic flow,” J. Spacecr. Rock., 32, 8 (1995).

    Google Scholar 

12. D.G. Levchuk, O.N. Ostapovich, and N.V. Pavlova, “Experimental data on the base heat transfer on conical bodies in hypersonic flow,” Kosmonavt. Raketostr., No. 11, 34 (1997).

    Google Scholar 

13. V. Zakkay and R. J. Cresci, “An experimental investigation of the near wake of a slender cone at M∞ = 8 and 12”, AIAA J., 4, 41 (1966).

    Google Scholar 

14. T. J. Hovarth, C. B. McGinley, and K. Hannemann, “Blunt body near-wake flow-field at Mach 6,” AIAA Paper, No. 1935 (1996).

15. B. R. Hollis and J.N. Perkins, “High-enthalpy aerothermodynamics of a Mars entry vehicle. Part 2. Computational results,” J. Spacecr. Rock., 34, 457 (1997).

    Google Scholar 

16. S. Yoon and A. Jameson, “A LU-SSOR scheme for the Euler and Navier-Stokes equations,” AIAA Paper, No. 0600 (1987).

17. T. H. Pulliam and J. L. Steger, “Recent improvements in efficiency, accuracy, and convergence for implicit approximate factorization algorithms,” AIAA Paper, No. 0360 (1985).

18. A. B. Gorshkov, “Calculation of the laminar base heat transfer downstream of slender cones,” Kosmonavt. Raketostr., No. 11, 13 (1997).

    Google Scholar 

19. V. I. Vlasov, “Method of calculation of a viscous shock layer with allowance for nonequilibrium physical and chemical processes,” Kosmonavt. Raketostr., No. 11, 5 (1997).

    Google Scholar 

20. R.V. Kovalev, ‘Calculation of two-dimensional turbulent supersonic flows past the lateral surface of a vehicle,” Kosmonavt. Raketostr., No. 11, 21 (1997).

    Google Scholar 

21. V. M. Kovenya and N.N. Yanenko, Splitting Method in Problems of Gas Dynamics [in Russian], Nauka, Novosibirsk (1981).

    Google Scholar 

22. A. B. Gorshkov, “Heat transfer in supersonic low-Re flow past a sphere and a cylinder,” Izv. Ross. Akad. Nauk, Mekh. Zhidk. Gaza, No. 1, 156 (2001).

    Google Scholar 

23. V. G. Artonkin, “Effect of cone bluntness on the base pressure at hypersonic velocities,” Uch. Zap. TsAGI, 8, No. 2, 106 (1977).

    Google Scholar 

24. W. K. Lockman, “Free-flight base pressure and heating measurements on sharp and blunt cones in a shock tunnel,” AIAA J., 5, 1898 (1967).

    Google Scholar 

25. J.A. Fay and F. R. Riddell, “Theory of stagnation point heat transfer in dissociated air,” J. Aeronaut. Sci., 25, 375 (1958).

    Google Scholar 

Download references