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Thrust Vectoring of Sonic Jet by Using Coanda Flap and Solenoid Valve

2016; American Institute of Aeronautics and Astronautics; Volume: 54; Issue: 9 Linguagem: Inglês

10.2514/1.j054993

1533-385X

Yeol Lee, Sanghoon Park, Younsoo Kim,

Computational Fluid Dynamics and Aerodynamics

No AccessTechnical NoteThrust Vectoring of Sonic Jet by Using Coanda Flap and Solenoid ValveYeol Lee, SangHoon Park and YounSoo KimYeol LeeKorea Aerospace University, Goyang 412-791, Republic of Korea*Professor, School of Aerospace and Mechanical Engineering, 200-1 Hwajeon-Dong. Senior Member AIAA (Corresponding Author).Search for more papers by this author, SangHoon ParkKorea Aerospace University, Goyang 412-791, Republic of Korea†Graduate Research Assistant, Graduate School, Department of Aerospace and Mechanical Engineering, 200-1 Hwajeon-Dong.Search for more papers by this author and YounSoo KimKorea Aerospace University, Goyang 412-791, Republic of Korea‡Undergraduate Student, Department of Aerospace and Mechanical Engineering, 200-1 Hwajeon-Dong.Search for more papers by this authorPublished Online:30 Jun 2016https://doi.org/10.2514/1.J054993SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Deere K. A., “Summary of Fluidic Thrust Vectoring Research Conducted at NASA Langley Research Center,” 21st AIAA Applied Aerodynamics Conference, AIAA Paper 2003-3800, June 2003. LinkGoogle Scholar[2] Wing D. J., “Static Investigation of Two Fluidic Thrust-Vectoring Concepts on a Two-Dimensional Convergent Divergent Nozzle,” NASA TM-4574, 1994. Google Scholar[3] Strykowski P. J., Krothapalli A. and Forliti D. J., “Counterflow Thrust Vectoring of Supersonic Jets,” AIAA Journal, Vol. 34, No. 11, 1996, pp. 2306–2314. LinkGoogle Scholar[4] Alvi F. S. and Strykowsk P., “Forward Flight Effects on Counterflow Thrust Vector Control of a Supersonic Jet,” AIAA Journal, Vol. 37, No. 2, 1999, pp. 279–281. LinkGoogle Scholar[5] Yagle P. J., Miller D. N., Gin K. B. and Hamstra J. W., “Demonstration of Fluidic Throat Skewing for Thrust Vectoring in Structurally Fixed Nozzles,” Journal of Fluid Engineering for Gas Turbines and Power, Vol. 123, No. 3, 2001, pp. 502–507. CrossrefGoogle Scholar[6] Mason M. S. and Crowther W. J., “Fluidic Thrust Vectoring for Low Observable Air Vehicle,” 2nd AIAA Flow Control Conference, AIAA Paper 2004-2210, June–July 2004. LinkGoogle Scholar[7] Flamm J. D., Deere K. A., Mason M. L., Berrier B. L. and Johnson S. K., “Design Enhancements of the Two-Dimensional, Dual Throat Fluidic Thrust Vectoring Nozzle Concept,” 3rd AIAA Flow Control Conference, AIAA Paper 2006-3701, June 2006. LinkGoogle Scholar[8] Saghafi F. and Banazadeh A., “Co-Flow Fluidic Thrust Vectoring Requirements for Longitudinal and Lateral Trim Purpose,” 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA Paper 2006-4980, July 2006. LinkGoogle Scholar[9] Neely A. J., Gesto F. N. and Young J., “Performance Studies of Shock Vector Control Fluidic Thrust Vectoring,” 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA Paper 2007-5086, July 2007. LinkGoogle Scholar[10] Clarke A. J., “The Conceptual Design of Novel Future UAV’s Incorporating Advanced Technology Research Components,” Ph.D. Dissertation, Cranfield Univ., Cranfield, England, U.K., 2011. Google Scholar[11] Song M. J., Park S. H. and Lee Y., “Application of Backstep Coanda Flap for Supersonic Coflowing Fluidic Thrust-Vector Control,” AIAA Journal, Vol. 42, No. 10, 2014, pp. 2355–2359. LinkGoogle Scholar[12] Santos M. M., “Experimental Study on Counter Flow Thrust Vectoring of a Gas Turbine Engine,” Ph.D. Dissertation, Florida State Univ., Tallahassee, FL, 2004. Google Scholar[13] Park S. H., Kwak J. Y., Chang H. B. and Lee Y., “Improving the Coanda Effect of the Sonic Jet by Utilizing Side Plates on the Flap,” Proceedings of the 7th Asia-Pacific International Symposium on Aerospace Technology, APISAT2015, Australia, Nov. 2015. Google Scholar[14] Song M. J., Chang H. B., Cho Y. H. and Lee Y., “Development of the High-Accuracy Multi-Component Balance for Fluidic Thrust Vectoring Nozzle of UAV,” Journal of the Korean Society for Aeronautical and Space Sciences, Vol. 41, No. 2, 2013, pp. 142–149. CrossrefGoogle Scholar[15] von Glahn U. H., “Use of the Coanda Effect for Jet Deflection and Vertical Lift with Multiple Flat Plate and Curved Plate Deflection Surfaces,” NACA TN-4377, 1958. Google Scholar Previous article Next article