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Yaw-Control Spoiler Design Using Design of Experiments Based Wind Tunnel Testing

2014; American Institute of Aeronautics and Astronautics; Volume: 52; Issue: 2 Linguagem: Inglês

10.2514/1.c032747

1533-3868

Byeong-Min Jeong, Dongoo Lee, Ho-Joon Shim, Jaemyung Ahn, Han‐Lim Choi, Seung-O Park, Se-Yoon Oh,

Aerospace and Aviation Technology

No AccessEngineering NoteYaw-Control Spoiler Design Using Design of Experiments Based Wind Tunnel TestingByeongmin Jeong, Dongoo Lee, Hojoon Shim, Jaemyung Ahn, Han-Lim Choi, Seung-O Park and Se-Yoon OhByeongmin JeongDepartment of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon 305-701, Republic of Korea*Research Assistant, Department of Aerospace Engineering, 291 Daehak-Ro.Search for more papers by this author, Dongoo LeeDepartment of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon 305-701, Republic of Korea*Research Assistant, Department of Aerospace Engineering, 291 Daehak-Ro.Search for more papers by this author, Hojoon ShimDepartment of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon 305-701, Republic of Korea*Research Assistant, Department of Aerospace Engineering, 291 Daehak-Ro.Search for more papers by this author, Jaemyung AhnDepartment of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon 305-701, Republic of Korea†Assistant Professor, Department of Aerospace Engineering, 291 Daehak-Ro; . Member AIAA (Corresponding Author).Search for more papers by this author, Han-Lim ChoiDepartment of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon 305-701, Republic of Korea‡Assistant Professor, Department of Aerospace Engineering, 291 Daehak-Ro. Member AIAA.Search for more papers by this author, Seung-O ParkDepartment of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon 305-701, Republic of Korea§Professor, Department of Aerospace Engineering, 291 Daehak-Ro. Member AIAA.Search for more papers by this author and Se-Yoon OhAgency for Defense Development, Daejeon 305-600, Republic of Korea¶Principal Researcher, The 1st R&D Institute. Member AIAA.Search for more papers by this authorPublished Online:15 Dec 2014https://doi.org/10.2514/1.C032747SectionsView Full TextPDFPDF Plus ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Landman D., Simpson J., Vicroy D. and Parker P., “Response Surface Methods for Efficient Complex Aircraft Configuration Aerodynamic Characterization,” Journal of Aircraft, Vol. 44, No. 4, 2007, pp. 1189–1195. doi:https://doi.org/10.2514/1.24810 JAIRAM 0021-8669 LinkGoogle Scholar[2] Montgomery D., Design and Analysis of Experiments, 7th ed., Wiley, Hoboken, NJ, 2009, pp. 135–172. Google Scholar[3] Myers R., Montgomery D. and Anderson-Cook C., “Response Surface Methodology: Process and Product Optimization Using Designed Experiments,” 3rd ed., Wiley, Hoboken, NJ, 2009, pp. 296–302. Google Scholar[4] Cummings R. and Schutte A., “Integrated Computational/Experimental Approach to Unmanned Combat Air Vehicle,” Journal of Aircraft, Vol. 49, No. 6, 2012, pp. 1542–1557. doi:https://doi.org/10.2514/1.C031430 JAIRAM 0021-8669 LinkGoogle Scholar[5] Schutte A., Hummel D. and Hitzel S., “Flow Physics of a Generic Unmanned Combat Aerial Vehicle Configuration,” Journal of Aircraft, Vol. 49, No. 6, 2012, pp. 1638–1651. doi:https://doi.org/10.2514/1.C031386 JAIRAM 0021-8669 LinkGoogle Scholar[6] Woolvin S., “UCAV Configuration and Performance Trade-Offs,” AIAA Paper 2006-1264, Jan. 2006. LinkGoogle Scholar[7] McParlin S., Bruce R., Hepworth A. and Rae A., “Low Speed Wind Tunnel Tests on the 1303 UCAV Concept,” AIAA Paper 2006-2985, June 2006. LinkGoogle Scholar[8] Arthur M. and Petterson K., “A Computational Study of the Low-Speed Flow over the 1303 UCAV Configuration,” AIAA Paper 2007-4568, June 2007. LinkGoogle Scholar[9] Brett J., Tang L., Hutchins N., Valiyff A. and Ooi A., “Computational Fluid Dynamics Analysis of the 1303 Unmanned Combat Air Vehicle,” Proceedings of the 17th Australasian Fluid Mechanics Conference, Auckland, Dec. 2010, pp. 341–344. Google Scholar[10] Chandrasekhara M. and McLain B., “Aerodynamic Studies over a Maneuvering UCAV 1303 Configuration,” Aeronautical Journal, Vol. 117, No. 1190, 2013, pp. 445–465. Google Scholar[11] Dorsett K. M. and Mehl D. R., “Innovative Control Effectors (ICE),” Lockheed Martin Tactical Aircraft Systems WL-TR-96-3043, Fort Worth, TX, 1996. Google Scholar[12] Bowlus J., Multhopp D. and Banda S., “Challenges and Opportunities in Tailless Aircraft Stability and Control,” AIAA Paper 1997-3830, Aug. 1997. LinkGoogle Scholar[13] Stenfelt G. and Ringertz U., “Lateral Stability and Control of a Tailless Aircraft Configuration,” Journal of Aircraft, Vol. 46, No. 6, 2009, pp. 2161–2164. doi:https://doi.org/10.2514/1.41092 JAIRAM 0021-8669 LinkGoogle Scholar[14] Stenfelt G. and Ringertz U., “Yaw Control of a Tailless Aircraft Configuration,” Journal of Aircraft, Vol. 47, No. 5, 2010, pp. 1807–1811. doi:https://doi.org/10.2514/1.C031017 JAIRAM 0021-8669 LinkGoogle Scholar[15] Stenfelt G. and Ringertz U., “Yaw Departure and Recovery of a Tailless Aircraft Configuration,” Journal of Aircraft, Vol. 50, No. 1, 2013, pp. 311–315. doi:https://doi.org/10.2514/1.C031868 JAIRAM 0021-8669 LinkGoogle Scholar[16] Landman D., Simpson J., Mariani R., Ortiz F. and Britcher C., “Hybrid Design for Aircraft Wind-Tunnel Testing Using Response Surface Methodologies,” Journal of Aircraft, Vol. 44, No. 4, 2007, pp. 1214–1221. doi:https://doi.org/10.2514/1.25914 JAIRAM 0021-8669 LinkGoogle Scholar[17] Rao S. S., Engineering Optimization: Theory and Practice, Wiley, Hoboken, NJ, 2009, pp. 422–428. CrossrefGoogle Scholar[18] Coleman T., Branch M. A. and Grace A., Optimization Toolbox: Users guide, Ver. 2, The MathWorks Inc., Natick, MA, 1999. Google Scholar Previous article