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The Effect of Canard Configurations to the Aerodynamics of the Blended Wing Body
Abstract:The aerodynamics characteristics of a blended-wing body (BWB) aircraft were obtained in Universiti Teknologi MARA low speed wind tunnel. The scaled-down of BWB model consisted of a canard as its horizontal stabilizer. There were four canards with different aspect ratio used in the experiments. Canard setting angles were varied from -20q to 20q. All tests were conducted at velocity of 35 m/s, with Mach number 0.1. At low angles of attacks, the increment of lift slope for various canards aspect ratio is small and almost constant. Higher canard aspect ratio will cause higher drag. However, canard has a high effect to the moment at zero lift, CM,0.The visualization using mini tuff was performed to observe the airflow at the upper surface of canard. KeywordsAerodynamics,blended-wing body, canard, wind tunnel.
Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1061098Procedia APA BibTeX Chicago EndNote Harvard JSON MLA RIS XML ISO 690 PDF Downloads 5223
References:1] Eugene. L.Tu, s Effect of canard Deflection on Close-Coupled Canard-Wing-Body Aerodynamics s, Journal of Aircraft, vol. 31, pp. 138-145, Jan-Feb 1994.
 Y. Guy, T.E. McLaughlin, J.A Morrow, " Effects of canard shape on the center of pressure of a generic missile configuration s, in 38th Aerospace Sciences Meeting and Exhibit,Reno,NV, 2000.
 B.-F. Ma, P.Q Liu, Y.Wei " Effects of Wing and Canard Sweep on Lift Enhancementof Canard Configurations ", Journal Of Aircraft, vol. 41, NovemberDecember 2004.
 M. R. Soltani, F. Askary, A.R. Davari, Arash Nayebzadeh, " Effects of Canard Position on Wing Surface Pressure ", Scientia Iranica, International Journal of Science and Technology, vol. 17, pp. 136-145, April 2010.
 Wirachman Wisnoe, Wahyu Kuntjoro, Firdaus Mohamad, Rizal E.M Nasir, Nor Fazira Reduan, Zurriati Mohd Ali, s Experimental Results Analysis for UiTM BWB Baseline-I and Baseline-II UAV Running at 0.1 Mach number s, Journal of Mechanics, Issue 2, Volume 4, 2010, ISSN: 1998-4448, pp. 23-32, included in ISI/SCI Web of Science and Web of Knowledge (http://www.naun.org/journals/mechanics/)
 Nor Fazira Reduan , Wirachman Wisnoe, Wahyu Kuntjoro , Rizal Effendy Mohd Nasir , Firdaus Mohamad, Zurriati M.A., sStudy of Aerodynamics Characteristic of BWB Baseline-II s, International Conference on Advances in Mechanical Engineering (ICAME), Selangor,Malaysia, 2010. ISBN: 9789673631865.
 Firdaus Mohamad, Wirachman Wisnoe, Wahyu Kuntjoro, Rizal E.M. Nasir, Zurriati M.Ali, Fazira Reduan, sExperiment Results of UiTMs Blended Wing Body (BWB) Baseline-II UAV using Low Speed Wind Tunnel s, International Conference on Advances in Mechanical Engineering (ICAME),Selangor,Malaysia, 2010. ISBN: 9789673631865.
 Rizal E. M. Nasir, Zurriati Mohd Ali, Wahyu Kuntjoro, Wirachman Wisnoe., s Investigation on Aerodynamic Characteristics of Baseline-II E-2 Blended Wing-Body Aircraft with Canard via Computational Simulation s, The International Meeting on Advances in Thermofluids (IMAT) Universiti Teknologi Malaysia, 2011.
 Zurriati Mohd Ali, Wahyu Kuntjoro, Wirachman Wisnoe, Rizal Efendy Mohd Nasir, Firdaus Mohamad, Nor F. Reduan, s The Aerodynamics Performance of Blended Wing Body Baseline-II E2s, International Conference on Computer and Communication Devices (ICCCD), Bali,Indonesia, 2011., ISBN: 978142449831, pp 293-297 included in IEEE Xplore, and indexed by Ei Compendex and Thomson ISI.
 Zurriati Mohd Ali, Wahyu Kuntjoro,Wirachman Wisnoe, Rizal E.M Nasir, s The Effect of Canard on Aerodynamics of Blended Wing Body s, Applied Mechanics and Materials Vols. 110-116 (2012) pp 4156-4160. Available:www.scientific.net,doi10.4028/www.scientific.net/AMM. 110-116.4156.