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Two aspects of the use of full-and partial-span Gurney flapsNIKOLIC, Vojin R.Journal of aircraft. 2007, Vol 44, Num 5, pp 1745-1748, issn 0021-8669, 4 p.Article

Aerodynamics life at Reynolds numbers below 7 × 104LAITONE, E. V.AIAA journal. 1996, Vol 34, Num 9, pp 1941-1942, issn 0001-1452Conference Paper

Wake integration to predict wing span loading from a numerical simulationMATHIAS, D. L; ROSS, J. C; CUMMINGS, R. M et al.Journal of aircraft. 1995, Vol 32, Num 5, pp 1165-1167, issn 0021-8669Article

Etude du décrochage instationnaire tridimensional sur une aile rectangulaire = Unsteady three-dimensional stall on a rectangular wingCOSTES, J. J.La Recherche aérospatiale. 1987, Num 4, pp 55-69, issn 0034-1223Article

Planform variations and aerodynamic efficiency of movable tip strakesNIKOLIC, Vojin R.Journal of aircraft. 2007, Vol 44, Num 1, pp 340-343, issn 0021-8669, 4 p.Article

Optimal rectangular end platesSTANDINGFORD, D. W. F; TUCK, E. O.Journal of aircraft. 1996, Vol 33, Num 3, pp 623-625, issn 0021-8669Article

Optimal scheduling of control surfaces on flexible wings to reduce induced dragKOLONAY, Raymond M; EASTEP, Franklin E.Journal of aircraft. 2006, Vol 43, Num 6, pp 1655-1661, issn 0021-8669, 7 p.Article

Effect of longitudinal riblets on the aerodynamic characteristics of a straight wingKONOVALOV, S. F; LASHKOV, YU. A; MIKHAILOV, V. V et al.Fluid dynamics. 1995, Vol 30, Num 2, pp 183-1187, issn 0015-4628Article

The representation of the pressure coefficient surface on the upper side of wedged rectangular wings in supersonic flowNASTASE, A; JAKOBS, R.Zeitschrift für angewandte Mathematik und Mechanik. 1994, Vol 74, Num 5, pp T470-T473, issn 0044-2267Article

Effect of flap motion on unsteady aerodynamic loadsLEE, T; GERONTAKOS, P.Journal of aircraft. 2007, Vol 44, Num 1, pp 333-337, issn 0021-8669, 5 p.Article

Effect of full-span Gurney flap height on wing wake vortex alleviationNIKOLIC, Vnjin R.Journal of aircraft. 2006, Vol 43, Num 5, pp 1555-1558, issn 0021-8669, 4 p.Article

Poststall prediction of multiple-lifting-surface configurations using a decambering approachMUKHERJEE, Rinku; GOPALARATHNAM, Ashok.Journal of aircraft. 2006, Vol 43, Num 3, pp 660-668, issn 0021-8669, 9 p.Article

Robustness of the subsonic doublet lattice methodVAN ZYL, L. H.Aeronautical Journal. 2003, Vol 107, Num 1071, pp 257-262, issn 0001-9240, 6 p.Article

Unsteady lifting surface theory in sonic flow : The problem revisitedSOVIERO, P. A. O; PINTO, F. H. L.AIAA journal. 2000, Vol 38, Num 5, pp 931-933, issn 0001-1452Article

Effects of wing-tip strakes on a sheared-tip wingTRAUB, L. W; GALLS, S. F; REDINIOTIS, O et al.Journal of aircraft. 1999, Vol 36, Num 6, pp 1055-1062, issn 0021-8669Article

Design, fabrication and testing of a new twist-active wing designBARRETT, R; LAW, D.SPIE proceedings series. 1998, pp 33-41, isbn 0-8194-2773-X, 2VolConference Paper

Effects of delta planform tip sails on the performance of a blunt edged rectangular wingTRAUB, L. W.Aeronautical Journal. 1997, Vol 101, Num 1002, pp 87-92, issn 0001-9240Article

Investigations of tip vortices with the triple hot-wire anemometryNOCKEMANN, M.Zeitschrift für Flugwissenschaften und Weltraumforschung. 1995, Vol 19, Num 6, pp 380-386, issn 0342-068XArticle

2D and 3D low frequency aerodynamicsVAN ZYL, L. H.Aeronautical Journal. 2008, Vol 112, Num 1136, pp 609-612, issn 0001-9240, 4 p.Article

Methods for calculating the subsonic aerodynamic center of finite wingsREDDEN, William P.Journal of aircraft. 2003, Vol 40, Num 5, issn 0021-8669, p. 1003Article

A constant pressure lifting line theory for subsonic flowJADIC, I.Revue roumaine des sciences techniques. Série de mécanique appliquée. 1993, Vol 38, Num 6, pp 643-650, issn 0035-4074Article

A summary of measurements of steady and oscillatory pressures on a rectangular wingMABEY, D. G; WELSH, B. L; PYNE, C. R et al.Aeronautical Journal. 1988, Vol 92, Num 911, pp 10-28, issn 0001-9240Article

The wing tip vortex system in a starting flowFREYMUTH, P; FATHI FINAISH; BANK, W et al.Zeitschrift für Flugwissenschaften und Weltraumforschung. 1986, Vol 10, Num 2, pp 116-118, issn 0342-068XArticle

Dynamics of revolving wings for various aspect ratiosGARMANN, D. J; VISBAL, M. R.Journal of fluid mechanics. 2014, Vol 748, pp 932-956, issn 0022-1120, 25 p.Article

First look into effects of discrete midspan vortex injection on wing performanceNIKOLIC, Vojin R; JUMPED, Eric J.Journal of aircraft. 2004, Vol 41, Num 5, pp 1177-1182, issn 0021-8669, 6 p.Article

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