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NTIS 바로가기한국항공우주학회지 = Journal of the Korean Society for Aeronautical & Space Sciences, v.50 no.5, 2022년, pp.297 - 308
김영진 (Department of Aerospace Engineering, Inha University) , 이형진 (Department of Aerospace Engineering, Inha University)
Most air-breathing aircraft operated in the hypersonic region are equipped with a scramjet engine. In a scramjet engine, a shock wave generated at an inlet acts as a compressor for a general gas turbine engine instead, so total pressure loss caused by the shock wave is considered very important. In ...
Lee, Y. J., Kang, S. H. and Yang, S. S., "Current Technological Trends in Hypersonic Flight with Air-Breathing Propulsion System," Current Industrial and Technological Trends in Aerospace, Vol. 7, No. 1, 2009, pp. 43~55.
Smart, M. K., "Scramjet Inlets," NATO Report RTO-EN-AVT-185 Lecture, 2010, pp. 9-1~24.
Van Wie, D. M. and Molder, S., "Applications of Busemann Inlet Design for Flight at Hypersonic Speeds," 1992 Aerospace Design Conference, February 1992, pp. 1210~1221.
Smart, M. K., "Design of Three-Dimensional Hypersonic Inlets with Rectangular-to-Elliptical Shape Transition," Journal of Propulsion and Power, Vol. 15, No. 3, 1999, pp. 408~416.
Tahir, R. B., Molder, S. and Timofeev, E. V., "Unsteady Starting of High Mach Number Air Inlets - A CFD Study," 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 2003, pp. 5191~5200.
Ramasubramanian, V., Starkey, R. and Lewis, R., "Numerical Simulations of Busemann Hypersonic Inlets at Finite Flight Angles," 26th AIAA Applied Aerodynamics Conference, August 2008, pp. 7497~7507.
Billig, F. S., Baurle, R. A., Tam, C. J. and Wornom, S. F., "Design and Analysis of Streamline Traced Hypersonic Inlets," 9th International Space Planes and Hypersonic Systems and Technologies Conference, November 1999, pp. 4974~4991.
Ramasubramanian, V., Lewis, R. and Starkey, R., "Performance of Various Truncation Strategies Employed on Hypersonic Busemann Inlets," 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, October 2009, pp. 7249~7263.
Ogawa, H., Russell, R. and Boyce, R., "Physical Insight into Scramjet Inlet Behavior via Multi-Objective Design Optimization," AIAA Journal, Vol. 50, No. 8, 2012, pp. 1773~1783.
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.
Flock, A. K. and Gulhan, A., "Viscous Effects and Truncation Effects in Axisymmetric Busemann Scramjet Intakes," AIAA Journal, Vol. 54, No. 6, 2016, pp. 1881~1891.
Billig, F. S. and Kothari, A. P., "Streamline Tracing: Technique for Designing Hypersonic Vehicles," Journal of Propulsion and Power, Vol. 16, No. 3, 2000, pp. 465~471.
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.
Tan, H. and Guo, R., "Experimental Study of the Unstable-Unstarted Condition of a Hypersonic Inlet at Mach 6," Journal of Propulsion and Power, Vol. 23, No. 4, 2007, pp. 783~788.
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.
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.
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.
Reinartz, B. U., "Performance Anaysis of a 3D Scramjet Intake," 26th International Congress of the Aeronautical Science, September 2008.
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.
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.
Saha, S. and Chakraborty, D., "Hypersonic Intake Starting Characteristics-A CFD Validation Study," Defence Science Journal, Vol. 62, No. 3, 2012, pp. 147~152.
Quan, L. H., Hung, N. P., Quang, L. D. and Long, V. L., "Anaysis and Design of a Scramjet Engine Inlet Operating from Mach 5 to Mach 10," International Journal of Mechanical Engineering and Applications, Vol. 4, No. 1, 2016, pp. 11~23.
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.
John, B. and Senthilkumar, P., "Alterations of Cowl Lip for the Improvement of Supersonic-Intake Performance," Journal of Applied Fluid Mechanics, Vol. 11, No. 1, 2018, pp. 31~41.
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.
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.
Zvegintsev, V. I. and Safonov, V. A., "Research of Characteristics of Isentropic Air Intake and Ducted Isentropic Air Intake," Frontiers in Aerospace Engineering, Vol. 4, No. 2, 2015, pp. 49~55.
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.
Oswatitsch, K., Contributions to the Development of Gasdynamics, Vieweg+Teubner Verlag, Wiesbaden, 1980, pp. 290~323.
Sarah, F., Birgit, U. R., Siegfried, M. and Marek, B., "Transition Prediction for Scramjets Using the γ-Re θt Model Coupled to Two Turbulence Models," Journal of Propulsion and Power, Vol. 31, No. 5, 2015, pp. 1~19.
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.
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.
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