kw.\*:("Leading edge")
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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
Hydrodynamics performance of hydrofoil-slat arrangements in 3D analysisYAVUZ, Tahir; KOC, Emre; KAYNAK, Bahadır et al.Energy conversion and management. 2013, Vol 75, pp 44-50, issn 0196-8904, 7 p.Article
Leading-edge redesign of a turbomachinery blade and its effect on aerodynamic performanceWEIHAO ZHANG; ZHENGPING ZOU; JIAN YE et al.Applied energy. 2012, Vol 93, pp 655-667, issn 0306-2619, 13 p.Article
The influence of leading-edge load alleviation on supersonic wing designDARDEN, C. M.Journal of aircraft. 1985, Vol 22, Num 1, pp 71-77, issn 0021-8669Article
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
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
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
Numerical simulation on impingement and film composite cooling of blade leading edge model for gas turbineZHAO LIU; LV YE; CHANGYEE WANG et al.Applied thermal engineering. 2014, Vol 73, Num 2, pp 1432-1443, issn 1359-4311, 12 p.Conference Paper
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
Fundamental aerodynamic characteristics of delta wings with leading-edge vortex flowsWOOD, R. M; MILLER, D. S.Journal of aircraft. 1985, Vol 22, Num 6, pp 479-485, issn 0021-8669Article
DESIGN OF FLAT PLATE LEADING EDYES TO AVOID FLOW SEPARATIONDAVIS MR.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 5; PP. 598-600; BIBL. 9 REF.Article
THE EFFECTS OF LEADING EDGE MODIFICATIONS ON THE POST-STALL CHARACTERISTICS OF WINGSWINKELMANN AE; BARLOW JB; SAINI JK et al.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 15 P.; BIBL. 18 REF.Conference Paper
A TRANSONIC PROPELLER OF TRIANGULAR PLAN FORM (AN EXTENSION)RIBNER HS.1978; U.T.I.A.S. TECH. NOTE; CAN; DA. 1978; NO 218; PP. 1-17; BIBL. 6 REF.; 7 ILL.Serial Issue
SINGULARITY AT THE TRAILING EDGE OF A SWEPT WINGCLAPWORTHY GJ.1979; A.I.A.A. J., NEW YORK; USA; DA. 1979; VOL. 17; NO 3; PP. 313-315; BIBL. 5 REF.Article
ON LIFT OF DELTA WINGS WITH LEADING-EDGE VORTICESHAYASHIDA M; SATO M; MATSUOKA K et al.1977; BULL. UNIV. OSAKA PREFECT., A; JPN; DA. 1977; VOL. 26; NO 2; PP. 37-51; BIBL. 19 REF.Article
AN ANALYSIS OF THE LEADING-EDGE SINGULARITY IN TRANSONIC SMALL-DISTURBANCE THEORYKEYFITZ BL; MELNIK RE; GROSSMAN B et al.1978; QUART. J. MECH. APPL. MATH.; GBR; DA. 1978; VOL. 31; NO 2; PP. 137-155; BIBL. 18 REF.Article
"SPILLED" LEADING-EDGE VORTEX EFFECTS ON DYNAMIC STALL CHARACTERISTICS.ERICSSON LE; REDING JP.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 4; PP. 313-315; BIBL. 16 REF.Article
EFFECT OF LEADING-EDGE VORTEX FLAPS ON AERODYNAMIC PERFORMANCE OF DELTA WINGSSUBBA REDDY C.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 9; PP. 796-798; BIBL. 8 REF.Article
STUDIES OF LEADING-EDGE THRUST PHENOMENACARLSON HW; MACK RJ.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 10 P.; BIBL. 14 REF.Conference Paper
Subcritical spatial transition of swept Hiemenz flowOBRIST, Dominik; HENNIGER, Rolf; KLEISER, Leonhard et al.International journal of heat and fluid flow. 2012, Vol 35, pp 61-67, issn 0142-727X, 7 p.Article
VORTEX LIFT PREDICTIONS FOR CAMBERED WINGS.SHEPSHELOVICH M.1976; ISRAEL J. TECHNOL.; ISRAEL; DA. 1976; VOL. 14; NO 1-4; PP. 18-22; BIBL. 6 REF.; (ISR. ANNU. CONF. AVIAT. ASTRONAUT. 18. PROC.; TEL AVIV-HAIFA; 1976)Conference Paper
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