Pascal and Francis Bibliographic Databases

Help

Search results

Your search

kw.\*:("Bord attaque")

Document Type [dt]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Publication Year[py]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Discipline (document) [di]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Language

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Author Country

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Origin

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Results 1 to 25 of 1186

  • Page / 48
Export

Selection :

  • and

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

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

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

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

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

THE LEADING EDGE EFFECT IN UNSTEADY NATURAL CONVECTION ON A VERTICAL PLATE WITH TIME-DEPENDENT SURFACE TEMPERATURE OR HEAT FLUX.MIZUKAMI K.1977; INTERNATION. J. HEAT MASS TRANSFER; G.B.; DA. 1977; VOL. 20; NO 9; PP. 981-989; ABS. FR. ALLEM. RUSSE; 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

Trajectory integration in vortical flowsMURMAN, E. M; POWELL, K. G.AIAA journal. 1989, Vol 27, Num 7, pp 982-984, issn 0001-1452Article

Optimum supersonic wings with subsonic leading edgesBOS, H. J.Journal of aircraft. 1986, Vol 23, Num 4, pp 326-332, issn 0021-8669Article

Assessment of preliminary prediction techniques for wing leading-edge vortex flows at supersonic speedsWOOD, R. M; MILLER, D. S.Journal of aircraft. 1985, Vol 22, Num 6, pp 473-478, issn 0021-8669Article

  • Page / 48