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Results 1 to 25 of 734

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Opportunities for the integrated use of measurements and computations for the understanding of delta wing aerodynamicsGURSUL, I; ALLAN, M. R; BADCOCK, K. J et al.Aerospace science and technology. 2005, Vol 9, Num 3, pp 181-189, issn 1270-9638, 9 p.Article

The International Vortex Flow Experiment 2 (VFE-2): Background, objectives and organization : Understanding and Modeling Vortical Flows to Improve the Technology Readiness Level for Military AircraftHUMMEL, Dietrich J.Aerospace science and technology (Imprimé). 2013, Vol 24, Num 1, pp 1-9, issn 1270-9638, 9 p.Conference Paper

ECOULEMENTS A DECOLLEMENT SUR UNE AILE CONIQUE CONCAVEKRAVETS VV; SHVETS AI.1983; IZVESTIJA AKADEMII NAUK SSSR. MEHANIKA ZIDKOSTI I GAZA; ISSN 0568-5281; SUN; DA. 1983; NO 2; PP. 83-91; BIBL. 12 REF.Article

Régime hypercritique de l'écoulement hypersonique autour d'une aile triangulaireDUDIN, G. N; LIPATOV, I. I.Prikladnaâ mehanika i tehničeskaâ fizika. 1985, Num 3, pp 100-106, issn 0869-5032Article

Computation of vortex breakdown on a rolling delta wingGORDNIER, R. E.Journal of aircraft. 1995, Vol 32, Num 3, pp 686-688, issn 0021-8669Conference Paper

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

Modeling effects on the prediction of aerodynamic performance of double-delta wingREDDY, C. S.Journal of aircraft. 1988, Vol 25, Num 1, pp 94-96, 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

Ecoulement autour des ailes delta à cassure du bord d'attaqueSHVETS, A. I.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1985, Num 1, pp 171-175, issn 0568-5281Article

The pitching delta wingMOHAMED GAD-EL-HAK; CHIH-MING HO.AIAA journal. 1985, Vol 23, Num 11, pp 1660-1665, issn 0001-1452Article

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

An optimality criterion method for structures with stress, displacement and frequency constraintsZACHAROPOULOS, A; WILLMER, K. D; KHAN, M. R et al.Computers & structures. 1984, Vol 19, Num 4, pp 621-629, issn 0045-7949Article

Flow over double delta wing and wing body at high αMANOR, D; WENTZ, W. H. JR.Journal of aircraft. 1985, Vol 22, Num 1, pp 78-82, issn 0021-8669Article

Vortex flow over delta and double-delta wingsHOEIJMAKERS, H. W. M; VAATSTRA, W; VERHAAGEN, N. G et al.Journal of aircraft. 1983, Vol 20, Num 9, pp 825-832, issn 0021-8669Article

Computational technique for compressible vortex flows post wings at large incidenceKANDIL, O. A.Journal of aircraft. 1985, Vol 22, Num 9, pp 750-755, issn 0021-8669Article

Etude numérique de l'échange de chaleur à la surface d'une aile delta dans un écoulement hypersonique d'air sous de grands angles d'attaqueAFONINA, N. E; VLASOV, A. YU; GROMOV, V. G et al.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1984, Num 5, pp 196-199, issn 0568-5281Article

Criteria for location of vortex breakdown over delta wingsGURSUL, I.Aeronautical Journal. 1995, Vol 99, Num 985, pp 194-196, issn 0001-9240Article

Development of an analytical model of wing rock for slender delta wingsELZEBDA, J. M; NAYFEH, A. H; MOOK, D. T et al.Journal of aircraft. 1989, Vol 26, Num 8, pp 737-743, issn 0021-8669, 7 p.Article

Measurements of ground effect for delta wingsKATZ, J; LEVIN, D.Journal of aircraft. 1984, Vol 21, Num 6, pp 441-443, issn 0021-8669Article

Optimisation des caractéristiques aérodynamiques des ailes delta aux vitesses de vol supersoniqueVORONIN, V. I; SHVETS, A. I.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1984, Num 5, pp 136-140, issn 0568-5281Article

Large CYBER 205 model of the Euler equations for vortex-stretched turbulent flow around delta wingsRIZZI, A; PURCELL, C. J.Engineering computations. 1985, Vol 2, Num 1, pp 63-70, issn 0264-4401Article

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

Calculation of nonlinear subsonic characteristics of wings with thickness and camber at high incidenceGORDON, R; ROM, J.AIAA journal. 1985, Vol 23, Num 6, pp 817-825, issn 0001-1452Article

OPTIMISATION DES STRUCTURES D'AVIONPETIAU C; LECINA G.1982; J. MEC. THEOR. APPL.; ISSN 0750-7240; FRA; DA. 1982; VOL. 1; NO 2; PP. 291-309; ABS. ENG; BIBL. 7 REF.Article

CALCULATION OF VORTEX BREAKDOWN LOCATIONS FOR FLOW OVER DELTA WINGS.WILSON JD.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 10; PP. 1020-1022; BIBL. 13 REF.Article

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