{"title":"Study of Aerodynamic Characteristics of the Unmanned Aircraft in the Wake","authors":"O. Solovyov, S. Eryomenko, V. Kobrin, V. Chmovzh","volume":77,"journal":"International Journal of Aerospace and Mechanical Engineering","pagesStart":897,"pagesEnd":901,"ISSN":"1307-6892","URL":"https:\/\/publications.waset.org\/pdf\/1104","abstract":"<p>The methodology of numerical simulation and calculation of aerodynamic characteristics of aircraft taking into account impact of wake on it has been developed. The results of numerical experiment in comparison with the data obtained in the wind tunnel are presented. Efficiency of methodology of calculation and the reliability of the results is shown.<\/p>\r\n","references":"[1] Belotserkovsky S.M., Nisht M.I. Separated and attached flow of thin\r\nwings by ideal fluid. - \u00f0\u00a3.: Science, 1978.\r\n[2] Hegen G.H. Wake encounter test in DNW wind tunnel - test number 98-\r\n1116, NLR-CR-98291 and WAVENC-TN10, 1998.\r\n[3] R. Heinrich \"Numerical Simulation of Wake-Vortex Encounters Using\r\nthe Chimera-Technique \", New Results in Numerical and Experimental\r\nFluid Mechanics III, Contributions to the 12th STAB\/DGLR\r\nSymposium Stuttgart, Germany 2000, pp. 74-81.\r\n[4] Frank Holz-aring, pfel, Thomas Gerz, Michael Frech, Andreas Dograve,\r\nand rnbrack. \"Wake Vortices in Convective Boundary Layer\r\nand Their Influence on Following Aircraft\", Journal of Aircraft, Vol. 37,\r\nNo. 6 (2000), pp. 1001-1007.\r\n[5] R. Struijs, G. Jonville, D. Darracq, and R. Heinrich. \"Inviscid\r\nComputation of Effect of Wake Vortices on a Scale-Model Airplane\",\r\nJournal of Aircraft, Vol. 40, No. 1 (2003), pp. 100-109.","publisher":"World Academy of Science, Engineering and Technology","index":"Open Science Index 77, 2013"}