참고문헌 (39)

1. Ahmed, M.Y.M. and Qin, N. (2010a), "Drag reduction using aerodisks for hypersonic hemispherical bodies", J. Spacecraft Rockets, 47(1), 62-81. https://doi.org/10.2514/1.46655. 

   상세보기

2. Ahmed, M.Y.M. and Qin, N. (2011b), "Recent advances in the aerothermodynamics of spiked hypersonic vehicles", Prog. Aerosp. Sci., 47(6), 425-449. https://doi.org/10.1016/j.paerosci.2011.06.001. 

   상세보기

3. Baldwin, B.S. and Lomax, H. (1978), "Thin layer approximation and algebraic model for separated turbulent flow", Proceedings of the 16th Aerospace Sciences Meeting, Huntsville, Alabama, U.S.A., January. 

4. Chang, P.L. (1970), Separation of Flow, Pergamon Press, Oxford, U.K. 

5. Chung, K.M., Chang, P.H. and Chang, K.C. (2014), "Effect of Reynolds number on compressible convex-corner flows", Adv. Aircraft Spacecraft Sci., 1(4), 443-454. http://doi.org/10.12989/aas.2014.1.4.443 

   상세보기

6. Daniels L.E. and Yoshihara, H. (1954), "Effect of the upstream influences of a shock wave at supersonic speeds in the presence of a separated boundary flows", WADC Tech. Rept., Wright Air Development Center, Air Research and Development Command, United States Air Force, U.S.A. 

7. Das, S., Kumar, P., Ralh, M.K., Rao, R.K.M. and Prasad, J.K. (2013), "Drag reduction of a hemispherical body adopting spike at supersonic speed", J. Aerosp. Sci. Technol., 65(4), 313-325. 

8. Deng, F., Liang, B., Xie, F. and Qin, N. (2017), "Spike effects on drag reduction for hypersonic lifting body", J. Spacecraft Rockets, 54(6), 1185-1195. https://doi.org/10.2514/1.A33865. 

   상세보기

9. Gerdroodbary, M.B. and Hosseinalipour, S.M. (2010), "Numerical simulation of hypersonic flow over highly blunted cones with spike", Acta Astronaut., 67(1-2), 180-193. https://doi.org/10.1016/j.actaastro.2010.01.026. 

   상세보기

10. Haupt, B.F. and Koenig, K. (1987), "Aerodynamic effects of probe-induced flow separation on bluff bodies at transonic Mach numbers", J. Spacecraft Rockets, 24(4), 327-333. https://doi.org/10.2514/3.25920. 

    상세보기

11. Hillje, E.R. and Nelson, R.L. (1993), "Ascent air data system results from space shuttle flight test program", NASA CR 2283. Document ID: 19840002058. 

12. Huang, W., Chen, Z., Yan, L., Yan, B. and Du, Z. (2019b), "Drag and heat flux reduction mechanism induced by the spike and its combinations in supersonic flows: A review", Prog. Aerosp. Sci., 105, 31-39. https://doi.org/10.1016/j.paerosci.2018.12.001. 

    상세보기

13. Huang, W., Li, L., Yan, L.Q. and Zhang, T.T. (2017a), "Drag and heat flux reduction mechanism of blunted cone and aerodisks" Acta Astronaut., 136,168-178. https://doi.org/10.1016/j.actaastro.2017.05.040. 

14. Jameson, A., Schmidt W. and Turkel, E. (1981), "Numerical solution of Euler equations by finite volume methods using Runge-Kutta time-stepping scheme", Proceedings of the 14th Fluid and Plasma Dynamics Conference, Palo Alto, California, U.S.A., June. 

15. Jones, J.J. (1952), "Flow separation from rods ahead of blunt nose at Mach number 2.72", NACA RM, L52E05a, Document ID: 19930087040, National Advisory Committee for Aeronautics. Langley Aeronautical Lab, Langley Field, Virginia, U.S.A. 

16. Kalimuthu, R., Mehta, R.C. and Rathakrishnan, E. (2019), "Measured aerodynamic coefficients of without and with spiked blunt body at Mach 6", Adv. Aircraft Spacecraft Sci., 6(3), 225-238. https://doi.org/10.12989/aas.2019.6.3.225. 

17. Mair W.A. (1952) "Experiments on separation of boundary layers on probes in front of blunt-nosed bodies in a supersonic air stream", Phil. Mag., 43(342), 695-716. https://doi.org/10.1080/14786440708520987. 

    

18. Mehta, R.C. (1997), "Numerical simulation of flow past spiked-nose heat shield", ASME-FED-SM 97-3293. 

19. Mehta, R.C. (1998), "Flowfield over bulbous heat shield in transonic and low supersonic speeds", J. Spacecraft Rockets, 35(1), 102-105. https://doi.org/10.2514/3.27004. 

    상세보기

20. Mehta, R.C. (2002), "Numerical analysis of pressure oscillations over axisymmetric spiked blunt bodies at Mach 6.80", Shock Waves, 11(6), 431-440. https://doi.org/10.1007/s001930200127. 

    상세보기

21. Mehta, R.C. (2010a), "Numerical simulation of the flowfield over conical, disk and flat spiked body at Mach 6", Aeronaut. J., 114(1154), 225-236. https://doi.org/10.1017/ S0001924000003675. 

    상세보기

22. Mehta, R.C. (2010b), "High speed flow field analysis for satellite launch vehicle and reentry capsule", J. Magnetohydrodyn. Plasma Space Res., 15(1), 51-99. 

23. Mehta, R.C. (2017), "Multi-block structured grid generation method for computational fluid dynamics", Scholars J. Eng. Technol., 5(8), 387-393. https://doi.org/10.21276/sjet. 

24. Mehta, R.C. and Jayachandran, T. (1997), "Navier-Stokes solution for a heat shield with and without a forward facing spike", Comput. Fluids, 26(7), 741-754. https://doi.org/10.1016/S0045-7930(97)00011-X. 

    상세보기

25. Menezes, V., Saravanan, S., Jagadeesh, G. and Reddy, K.P.J. (2009b), "Aerodynamic drag reduction using aerospike for large angle blunt cone flying at hypersonic Mach number", Proceedings of the 22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, St. Louis, Missouri, U.S.A., June. 

26. Mikhail, A.G. (1991), "Spike-nosed projectiles: Computations and dual flow modes in supersonic flight", J. Spacecraft Rockets, 28(3), 418-424. https://doi.org/10.2514/3.26261. 

    상세보기

27. Milicov, S.S. and Parlevic, D.M. (2002), "Influence of spike shape at supersonic flow past nosed bodies: Experimental study", AIAA J., 40(5), 1018-1020. https://doi.org/10.2514/2.1745. 

    상세보기

28. Panaras, D. and Drikakis, D. (2009), "High speed unsteady flows around spiked-blunt bodies", J. Fluid Mech., 632, 69-96. https://doi.org/10.1017/ S0022112009006235. 

    상세보기

29. Piland, R.O. and Putland, L.W. (1954), "Zero-lift drag of several conical and blunt nose shapes obtained in free flight at Mach number of 0.7 to 1.3", NACA RM L54A27, Document Id: 19930089303, NACA Washington, U.S.A. 

30. Purohit, S.C. (1986), "A Navier-Stokes solution for a bulbous payload shroud", J. Spacecraft Rockets, 23(6), 590-596. https://doi.org/10.2514/3.25852. 

    상세보기

31. Sahoo, D., Das, S., Kumar, P. and Prasad, J.K. (2016), "Effect of spike on steady and unsteady flow over a blunt body at supersonic speed", Acta Astronaut., 128, 521-533. https://doi.org/10.1016/j.actaastro.2016.08.005. 

    상세보기

32. Sebastian, J.J., Suryan, A. and Kim, H.D. (2016), "Numerical analysis of hypersonic flow past blunt bodies with aerospikes", J. Spacecraft Rockets, 53(4), 669-677. https: //doi.org/10.2514/1.A33414. 

    상세보기

33. Shoemaker, J.M. (1990), "Aerodynamic spike flowfields computed to select optimum configuration at Mach 2.5 with experimental validation", Proceedings of the 28th Aerospace Sciences Meeting, Reno, Nevada, U.S.A., January. 

34. Srulijes, J., Runne, K. and Seiler, F. (2000), "Flow visualization and pressure measurements on spike-tipped blunt body", Proceedings of the 1st Aerodynamic Measurement Technology and Ground Testing Conference. 

35. Venkateshan, M., Kannamanimuthu, N., Das, S., Kumar, P. and Prasad, J.K. (2011), "Flowfield investigation over a hemispherical blunt body with different spikes at supersonic speed", Proceedings of the 38th National Conference on Fluid Mechanics and Fluid Power, Bhopal, India, December. 

36. Wang, Z.G., Sun, X.W., Huang, W., Li, S.B. and Yan, L. (2016), "Experimental investigation on drag and heat flux reduction in supersonic/hypersonic flows, A review", Acta Astronaut., 129, 95-110. https://doi.org/10.1016/j.actaastro.2016.09.004. 

    상세보기

37. White, J.T. (1993), "Application of Navier-Stokes flowfield analysis in the thermodynamic design of an aerospike configuration missile", Proceedings of the California AIAAIAHS/ASEE Aerospace Design Conference. 

38. Yadav, R. and Guven, U. (2013), "Aerothermodynamics of a hypersonic projectile with a double-disk aerospike", Aeronaut. J., 117(1195), 913-928. https://doi.org/10.1017/ S0001924000008587. 

    상세보기

39. Yamauchi, M., Fujii, K., Tamura, Y. and Higashino, F. (1995), "Numerical investigation of supersonic flows around a spiked blunt body", J. Spacecraft Rockets, 32(1), 32-42. https://doi.org/10.2514/3.26571. 

    상세보기