참고문헌 (43)

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11. Ogawa, H., Boyce, R. and Molder, S., "Effects of Leading-Edge Truncation and Stunting on Drag and Efficiency of Busemann Intakes for Axisymmetric Scramjet Engines," Journal of Fluid Science and Technology, Vol. 8, No. 2, 2013, pp. 186~199. 

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14. Smart, M. K., "Experimental Testing of a Hypersonic Inlet with Rectangular-to-Elliptical Shape Transition," Journal of Propulsion and Power, Vol. 17, No. 2, 2001, pp. 276~283. 

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16. Li, N., Chang, J., Jiang, C., Yu, D., Bao, W., Song, Y. and Jiao, X., "Unstart/Restart Hysteresis Characteristics Analysis of An Over-Under TBCC Inlet caused by Backpressure and Splitter," Aerospace Science and Technology, Vol. 72, 2018, pp. 418~425. 

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17. Saravanan, R., Desikan, S. L. N., Francise, K. J. and Kalimuthu, R., "Experimental Investigation of Start/Unstart Process during Hypersonic Intake at Mach 6 and its Control," Aerospace Science and Technology, Vol. 113, 2021, 106688. 

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18. Haberle, J. and Gulhan, A., "Internal Flowfield Investigation of a Hypersonic Inlet at Mach 6 with Bleed," Journal of Propulsion and Power, Vol. 23, No. 5, 2007, pp. 1007~1017. 

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19. Reinartz, B. U., "Performance Anaysis of a 3D Scramjet Intake," 26th International Congress of the Aeronautical Science, September 2008. 

20. Raj, N. O. P. and Venkatasubbaiah, K., "A New Approach for the Design of Hypersonic Scramjet Inlets," Physics of Fluids, Vol. 24, No. 8, 2012, pp. 086103-1~15. 

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21. Ding, F., Liu, J., Huang, W., Zhou, Y. and Guo, S., "Boundary-layer Viscous Correction Method for Hypersonic Forebody/Inlet Integration," Acta Astronautica, Vol. 189, 2021, pp. 638~657. 

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22. Saha, S. and Chakraborty, D., "Hypersonic Intake Starting Characteristics-A CFD Validation Study," Defence Science Journal, Vol. 62, No. 3, 2012, pp. 147~152. 

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24. Rajashree, V., Manivannan, P. and Kumar, G. D., "Computational Analysis of Scramjet Inlet," 2014 IEEE International Conference on Innovations in Engineering and Technology, March 2014, pp. 2730~2734. 

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26. Matthews, A. J., Jones, T. V. and Cain, T. M., "Design and Test of a Hypersonic Isentropic- Spike Intake with Aligned Cowl," Journal of Propulsion and Power, Vol. 21, No. 5, 2005, pp. 838~843. 

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27. Slater, J. W., "Design and Analysis Tool for External-Compression Supersonic Inlets," 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, January 2012, pp. 0016~0028. 

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29. Chen, H., Tan, H. J., Chang, Q. F. and Zhang, Y., "Buzz Flows in an External-Compression Inlet with Partially Isentropic Compression," AIAA Journal, Vol. 55, No. 12, 2017, pp. 4286~4295. 

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30. Kim, C. H. and Jeung, I. S., "Optimal Design of Two-Dimensional Hypersonic Intake Geometry," Journal of The Korean Society of Propulsion Engineers, Vol. 18, No. 6, 2014, pp. 1~10. 

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31. Kang, S. H., "Variable Inlet Design for Hypersonic Engines with a Wide Range of Flight Mach Numbers," Journal of The Korean Society of Propulsion Engineers, Vol. 19, No. 3, 2015, pp. 65~72. 

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32. Heo, Y., Moon, K. H. and Sung, H. G., "Investigation of Oswatitsch Scheme for Maximum Total Pressure Recovery of Hypersonic Wedge-type Intakes," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 45, No. 12, 2017, pp. 1031~1038. 

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33. Lee, K. J., Kang, S. H., Yang, S. S. and Park, C., "Conceptual Design Study of Two-Stage Hypersonic Scramjet Vehicle," Journal of The Korean Society of Propulsion Engineers, Vol. 16, No. 1, 2012, pp. 16~24. 

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34. Choi, J. H., Cheon, S. M., Choe, Y. H., Hong, W. R. and Kim, C. A., "Study on Concept Design of Supersonic Inlet and Flow Control of Bleeding under Operating Condition," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 40, No. 12, 2012, pp. 1025~1031. 

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35. Yang, I. Y., Lee, Y. J., Kim, Y. M. and Lee, K. J., "Combustion Test of a Mach 5 Scramjet Engine Model," Journal of The Korean Society of Propulsion Engineers, Vol. 17, No. 3, 2013, pp. 9~14. 

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36. Park, J. W., Park, I. S., Jin, S. W., Park, K. H. and Hwang, K. Y., "Investigation of the Intake Stability of Bank-to-Turn Supersonic Missile under Sideslip Angle Based on CFD Analysis," Journal of The Korean Society of Propulsion Engineers, Vol. 18, No. 3, 2014, pp. 8~16. 

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37. Jung, S. Y., Lee, J. H. and Kim, M. G., "Additive Drag Computation of Supersonic Inlet by Numerical Analysis on Inviscid Flow," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 43, No. 5, 2015, pp. 387~395. 

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38. Cha, S. W., Roh, T. S. and Lee, H. J., "Comparison of Performance on Hypersonic Intakes in Off-Design Conditions Through Numerical Simulations," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 47, No. 3, 2019, pp. 195~203. 

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39. Han, S. E., Shin, H. C. and Park, S. H., "Aerodynamic Model Development for Three-dimensional Scramjet Model Based on Two-dimensional CFD Analysis," Journal of The Korean Society of Propulsion Engineers, Vol. 24, No. 5, 2020, pp. 65~76. 

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42. Samuel, E. O., Charles, J. T. and John, W. S., "Inward-Turning Streamline-Tracing Inlet Design Method for Low-Boom, Low-Drag Applications," Journal of Propulsion and Power, Vol. 32, No. 5, 2016, pp. 1178~1189. 

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43. Li, Y., Zheng, X., Shi, C. and You, Y., "Integration of Inward-Turning Inlet with Airframe based on Dual-Waverider Concept," Aerospace Science and Technology, Vol. 107, 2020, pp. 1~9.