참고문헌 (17)

1. Fay, J. A. and Riddell, F. R., "Theory of Stagnation Point Heat Transfer in Dissociated Air", Journal of the Aeronautical Sciences, Vol. 25, No. 2, 1958, pp. 73-85. 

2. Moretti, G. and Abbett, M., "A Time-Dependent Computational Method for Blunt Body Flows", AIAA Journal, Vol. 4, No. 12, 1966, pp. 2136-2141. 

   상세보기

3. Kao, H. C., "Hypersonic Viscous Flow near the Stagnation Streamline of a Blunt Body: I. A Test of Local Similarity", AIAA Journal, Vol. 2, No. 11, 1964, pp. 1892-1897. 

   상세보기

4. Jain, A. C. and Adimurthy, V., "Hypersonic Merged Stagnation Shock Layers Part I: Adiabatic Wall Case", AIAA Journal, Vol. 12, No. 3, 1974, pp. 342-347. 

   상세보기

5. Klomfass, A. and Muller, S., "Calculation of a Stagnation Streamline Quantities in Hypersonic Blunt Body Flows", Shock Waves, Vol. 7, 1997, pp. 12-23. 

6. William, J., Verant, J. and Sagnier, P., "An Efficient Numerical Tool for Blunted Bodies Stagnation Line Rebuilding with Weakly Ionized Thermochemical Nonquilibrium flows", 15th IMACS-World Congress on Scientific Computation, Modeling and Applied Mathematics, Vol. 3, 1997, pp. 187-192. 

7. Billig, F. S., "Shock Wave Shapes around Spherical and Cylindrical Nosed Bodies", Journal of Spacecraft and Rockets, Vol. 4, No. 6, 1967, pp. 822-823. 

   상세보기

8. Lee, C. H., "Numerical Solution of Hypersonic Flow along the Stagnation Streamline of Blunt Body", The 2015 World Congress on Aeronautics, Nano, Bio, Robotics, and Energy, Incheon, Korea, August, 2015. 

9. Anderson, E. C. and Moss, J. N., "Numerical Solution of the Hypersonic Viscous Shock Layer Equations for Laminar, Transitional, and Turbulent Flows of a Perfect Gas over Blunt Axially Symmetric Bodies", NASA TN D-7865, 1975. 

10. Lee, C. H. and Park, S. O., "Computations of Hypersonic Flows over Blunt Body using a Modified Low-Diffusion Flux-Splitting Scheme", CFD Journal, Vol. 10, No. 4, 2002, pp. 490-500. 

    상세보기

11. Anderson, W. K., Thomas, J. L. and Van Leer, B., "Comparison of Finite Volume Flux Vector Splitting for the Euler equations", AIAA Journal, Vol. 24, No. 9, 1986, pp. 1453-1460. 

    상세보기

12. Steger, J. L. and Warming, R. F., "Flux Vector Splitting of the Inviscid Gas dynamics Equations with Application to Finite Difference Methods", Journal of Computational Physics, Vol. 40, No. 2, 1981, pp. 263-293. 

    상세보기

13. Tysinger, T. L. and Caughy, D. A., "Implicit Multigrid Algorithm for the Navier-Stokes Equations", AIAA Paper 91-0242, 1991. 

14. Rawat, P. S. and Zhong, X., "On High-Order Shock Fitting and Front Tracking Schemes for Numerical Simulation of Shock Disturbance Interactions", Journal of Computational Physics, Vol. 229, No. 19, 2010, pp. 6744-6780. 

    상세보기

15. Henrick, A. K., Aslam, T. D. and Powers, J. P., "Simulations of Pulsating One-Dimensional Detonations with True Fifth Order Accuracy", Journal of Computational Physics, Vol. 213, No. 1, 2006, pp. 311-329. 

    상세보기

16. Cleary, J. W., "Effects of Angle of Attack and Bluntness on Laminar Heating-Rate Distributions of a $15^{\circ}$ Cone at a Mach Number of 10.6", NASA TN D-5450, 1969. 

17. Lee, C. H. and Park, S. O., "Comparison of Time Implicit Symmetric Gauss-Seidel Iterative Schemes for Computation of Hypersonic Nonequilibrium Flow", KSAS International Journal, Vol. 2, No. 1, 2001, pp. 1-11. 

    원문보기 상세보기

저자의 다른 논문 :

이창호 (14)