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CASCADE WITH SUBSONIC LEADING-EDGE LOCUS.GOLDSTEIN ME.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 8; PP. 1117-1119; BIBL. 3 REF.Article

Engineering analysis of drooped leading-edge wings near stallTAE HWAN CHO; ANDERSON, J. D. JR.Journal of aircraft. 1984, Vol 21, Num 6, pp 446-448, issn 0021-8669Article

Slender wings with leading-edge vortex separation: a challenge for panel methods and Euler solversHITZEL, S. M; SCHMIDT, W.Journal of aircraft. 1984, Vol 21, Num 10, pp 751-759, issn 0021-8669Article

Combustion structures in lifted ethanol spray flamesMARLEY, Stephen K; WELLE, Eric J; LYONS, Kevin M et al.Journal of engineering for gas turbines and power. 2004, Vol 126, Num 2, pp 254-257, issn 0742-4795, 4 p.Article

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

Drag of wings with cambered airfoils and partial leading-edge suctionDELAURIER, J.Journal of aircraft. 1983, Vol 20, Num 10, pp 882-886, issn 0021-8669Article

An attached flow design of a noninterfering leading-edge extension to a thick delta wingFARHAD GHAFFARI; LAMAR, J. E.Journal of aircraft. 1986, Vol 23, Num 3, pp 237-243, issn 0021-8669Article

STUDIES OF LEADING-EDGE THUST PHENOMENACARLSON HW; MACK RJ.1980; J. AIRCR.; ISSN 0021-8669; USA; DA. 1980; VOL. 17; NO 12; PP. 890-897; BIBL. 14 REF.Article

AUGMENTATION OF VORTEX LIFT BY SPANWISE BLOWING.CAMPBELL JF.1975; IN: AM. INST. AERONAUT. ASTRONAUT AIRCR. SYST. TECHNOL. MEET.; LOS ANGELES; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 993; PP. 1-6; H.T. 3; BIBL. 19 REF.Conference Paper

Combined damage detection techniquesVANLANDUIT, S; PARLOO, E; GUILLAUME, P et al.Journal of sound and vibration. 2003, Vol 266, Num 4, pp 815-831, issn 0022-460X, 17 p.Article

TRANSONIC EQUIVALENCE RULE: A NONLINEAR PROBLEM INVOLVING LIFT.CHENG HK; HAFEZ MM.1975; J. FLUID MECH.; G.B.; DA. 1975; VOL. 72; NO 1; PP. 161-187; BIBL. 1 P. 1/2Article

TRAGENDE SCHNABELPROFILE IN STOSSFREIER SCHALLANSTROEMUNG. = PROFILS PORTANTS A BORDS D'ATTAQUE AIGUS DANS UN ECOULEMENT INCIDENT TRANSSONIQUE SANS CHOCSOBIECZKY H.1975; Z. ANGEW. MATH. PHYS.; SCHWEIZ; DA. 1975; VOL. 26; NO 6; PP. 819-830; ABS. ANGL.; BIBL. 4 REF.Article

FREE CONVECTION HEAT TRANSFER NEAR LEADING EDGE OF SEMI-INFINITE VERTICAL FLAT PLATE WITH FINITE THICKNESS (1ST. REPORT, ISOTHERMAL FLAT PLATE, PR=0.72)MIYAMOTO M; AKIYOSHI T.1981; BULL. JSME; ISSN 0021-3764; JPN; DA. 1981; VOL. 24; NO 197; PP. 1945-1952; BIBL. 15 REF.Article

High-incidence airfoil aerodynamics improvement by leading-edge oscillating flapHSIAO, F. B; LIANG, P. F; HUANG, C. Y et al.Journal of aircraft. 1998, Vol 35, Num 3, pp 508-510, issn 0021-8669Article

Experimental study of vortex flow control on double-delta wings using filletsHEBBAR, S. K; PLATZER, M. F; ALKHOZAM, A. M et al.Journal of aircraft. 1996, Vol 33, Num 4, pp 743-751, issn 0021-8669Conference Paper

Analysis of a delta wing with leading-edge flapsSEJONG OH; TAVELLA, D.Journal of aircraft. 1987, Vol 24, Num 6, pp 353-354, issn 0021-8669Article

Vortices incident upon a leading edge: instantaneous pressure fieldsRUHI KAYKAYOGLU; ROCKWELL, D.Journal of Fluid Mechanics. 1985, Vol 156, pp 439-461, issn 0022-1120Article

Prediction of leading-edge vortex behaviour to supplement the suction analogyRILEY, N; SMITH, J. H. B.Journal of engineering mathematics. 1985, Vol 19, Num 2, pp 157-172, issn 0022-0833Article

Etude numérique de la couche de choc visqueuse hypersonique sur des ailes d'envergure infinie avec un écoulement à angle d'attaque et à glissementGERSHBEJN, EH. A; SHCHELIN, V. S; YUNITSKIJ, S. A et al.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1984, Num 2, pp 104-108, issn 0568-5281Article

Effect of structural factors on maximum aerodynamic heat flux of strut leading surfaceWEN BAO; YOUHAI ZONG; JUNTAO CHANG et al.Applied thermal engineering. 2014, Vol 69, Num 1-2, pp 188-198, issn 1359-4311, 11 p.Article

New pair of leading-edge vortex structure for flow over delta wingJINJUN WANG; JINGXIA ZHAN.Journal of aircraft. 2005, Vol 42, Num 3, pp 718-721, issn 0021-8669, 4 p.Article

Leading edge noise from thick foils in turbulent flowsGERSHFELD, Jonathan.The Journal of the Acoustical Society of America. 2004, Vol 116, Num 3, pp 1416-1426, issn 0001-4966, 11 p.Article

Benefit and performance of various vortex flap configurationsRINOIE, Kenichi.Journal of aircraft. 2003, Vol 40, Num 6, pp 1215-1218, issn 0021-8669, 4 p.Article

Prediction of vortex lift of non-planar wings by the leading-edge suction analogyHARDY, B. C; FIDDES, S. P.Aeronautical Journal. 1988, Vol 92, Num 914, pp 154-164, issn 0001-9240Article

Effect of a round airfoil nose on leading-edge suctionLAN, C. E; INGCHUNG SU.Journal of aircraft. 1987, Vol 24, Num 7, pp 472-474, issn 0021-8669Article

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