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Experimental investigation of airfoil trailing edge heat transfer and aerodynamic lossesBRUNDAGE, A. L; PLESNIAK, M. W; LAWLESS, P. B et al.Experimental thermal and fluid science. 2007, Vol 31, Num 3, pp 249-260, issn 0894-1777, 12 p.Article

Effet de diffusion longitudinale au bord de fuite d'un anémomètre d'électrodiffusionVAJN, O; WEIN, O; KOVALEVSKAYA, N. D et al.Collection of Czechoslovak chemical communications. 1987, Vol 52, Num 3, pp 634-647, issn 0010-0765Article

Effect of angle of attack on rotor trailing-edge noiseCHOU, S.-T; GEORGE, A. R.AIAA journal. 1984, Vol 22, Num 12, pp 1821-1823, issn 0001-1452Article

Roll up of strake leading/trailing-edge vortex sheets for double-delta wingsYIN XIEYUAN.Journal of aircraft. 1985, Vol 22, Num 1, pp 87-89, issn 0021-8669Article

A class of airfoils having finite trailing-edge pressure gradientsORMSBEE, A. I; MAUGHMER, M. D.Journal of aircraft. 1986, Vol 23, Num 2, pp 97-103, issn 0021-8669Article

Indicial coefficients for a cropped delta wing in incompressible flowSTARK, V. J. E.Journal of aircraft. 1986, Vol 23, Num 5, pp 370-375, issn 0021-8669Article

Ein Modell zur analytischen Beschreibung von Randwirbeln = Modèle de description analytique de tourbillons de bord = An analytical model for describing edge vorticesSTAUFENBIEL, R.Zeitschrift für Flugwissenschaften und Weltraumforschung. 1985, Vol 9, Num 5, pp 283-293, issn 0342-068XArticle

TRANSFORMATION CONFORME REGULIEREMENT EXACTE DE L'EXTERIEUR D'UN CERCLE EN CONTOUR D'AILEMONAKHOV NM.1977; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1977; VOL. 20; NO 2; PP. 94-98; BIBL. 2 REF.Article

THE EFFECT OF TRAILING-EDGE STRIPS ON THE UNSTEADY AERODYNAMIC FORCES ON A CONTROL SURFACELONG G; FARRELL PA.1980; AERONAUT. J.; ISSN 0001-9240; GBR; DA. 1980; VOL. 84; NO 838; PP. 388-391; BIBL. 5 REF.Article

Compatibility of transonic flows at thick trailing edge in turbine blade rowINOUE, M; HAYASHI, H; YAMAGUCHI, S et al.Bulletin of the JSME. 1983, Vol 26, Num 221, pp 1877-1883, issn 0021-3764Article

Investigation of the possibilites of trailing edge shock waves intensity reduction by means of the edge geometry modificationDOERFFER, P.Archives of Mechanics. 1983, Vol 35, Num 1, pp 107-116, issn 0373-2029Article

Ecoulement turbulent d'un fluide près du bord de fuite d'une plaque avec un angle d'attaque nulVELICHKO, S. A; LIFSHITS, YU. B.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1983, Num 6, pp 17-23, issn 0568-5281Article

Experimental results for Reynolds number effects on trailing vorticesLEE, H; SCHETZ, J. A.Journal of aircraft. 1985, Vol 22, Num 2, pp 158-160, issn 0021-8669Article

Eddy viscosity models for wakes and separated flowsSRINIVAS, K; FLETCHER, C. A. J.AIAA journal. 1984, Vol 22, Num 1, pp 147-148, issn 0001-1452Article

Vortex shedding from a two-dimensional blunt trailing edge with unequal external free-stream velocitiesTAMURA, H; KIYA, M; ARIE, M et al.Bulletin of the JSME. 1984, Vol 27, Num 231, pp 1866-1872, issn 0021-3764Article

ANALYSIS OF CIRCULATION CONTROLLED AIRFOILS.GIBBS EH; NESS N.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 2; PP. 158-160; BIBL. 12 REF.Article

Effects of trailing wall modifications on cavity wall pressureYIN YIN PEY; LEOK POH CHUA.Experimental thermal and fluid science. 2014, Vol 57, pp 250-260, issn 0894-1777, 11 p.Article

Computational modeling of vortex breakdown control on a delta wingVLAHOSTERGIOS, Z; MISSIRLIS, D; YAKINTHOS, K et al.International journal of heat and fluid flow. 2013, Vol 39, pp 64-77, issn 0142-727X, 14 p.Article

NADDZWIEKOWY PRZEPLYW W OBSZARZE WYLOTOWYM DOSRODKOWEGO WIENCA KIERUJACEGO = ECOULEMENT DE SORTIE SUPERSONIQUE DANS UNE CASCADE DE PROFIL CENTRIPETELEBRECHT J.1981; MECH. TEOR. STOS.; ISSN 0079-3701; POL; DA. 1981; VOL. 19; NO 1; PP. 137-151; ABS. RUS/ENG; BIBL. 9 REF.Article

CORRELATION OF TURBULENT TRAILING VORTEX DECAY DATA.IVERSEN JD.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 5; PP. 338-342; BIBL. 19 REF.Article

Airfoil self noise reduction by non-flat plate type trailing edge serrationsCHONG, T. P; JOSEPH, P. F; GRUBER, M et al.Applied acoustics. 2013, Vol 74, Num 4, pp 607-613, issn 0003-682X, 7 p.Article

Numerical modeling of the vortex breakdown phenomenon on a delta wing with trailing-edge jet-flapKYRIAKOU, Marilena; MISSIRLIS, Dimitrios; YAKINTHOS, Kyros et al.International journal of heat and fluid flow. 2010, Vol 31, Num 6, pp 1087-1095, issn 0142-727X, 9 p.Conference Paper

Acoustic and aerodynamic design and characterization of a small-scale aeroacoustic wind tunnelSARRADJ, Ennes; FRITZSCHE, Christoph; GEYER, Thomas et al.Applied acoustics. 2009, Vol 70, Num 8, pp 1073-1080, issn 0003-682X, 8 p.Article

Influence of trailing-edge flow control on airfoil performanceGAI, S. L; PALFREY, R.Journal of aircraft. 2003, Vol 40, Num 2, pp 332-337, issn 0021-8669, 6 p.Article

Experimental and theoretical study of wings with blunt trailing edgesRAMJEE, V; TULAPURKARA, E. G; BALABASKARAN, V et al.Journal of aircraft. 1986, Vol 23, Num 4, pp 349-352, issn 0021-8669Article

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