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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

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

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

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

Experimental studies of vortex flaps and vortex platesRINOIE, K; STOLLERY, J. L.Journal of aircraft. 1994, Vol 31, Num 2, pp 322-329, issn 0021-8669Conference Paper

Breakdown analysis on delta wing vorticesGUGLIERI, G; ONORATO, M; QUAGLIOTTI, F et al.Zeitschrift für Flugwissenschaften und Weltraumforschung. 1992, Vol 16, Num 4, pp 226-230, issn 0342-068XArticle

Nonlinear aerodynamics of a delta wing in combined pitch and rollER-EL, J; SETER, D; WEIHS, D et al.Journal of aircraft. 1989, Vol 26, Num 3, pp 254-259, issn 0021-8669Article

Hydrodynamic modification of the horseshoe vortex at a vertical pier junction with groundGUPTA, A. K.The Physics of fluids. 1987, Vol 30, Num 4, pp 1213-1215, issn 0031-9171Article

Quasi-transonic flow past delta wingsSCHLEINIGER, G.Quarterly of applied mathematics. 1987, Vol 45, Num 2, pp 265-277, issn 0033-569XArticle

Evolution of vortical structure over delta-wing with transient along-core blowingKUO, C.-H; LU, N.-Y; LIN, D.-C et al.AIAA journal. 1997, Vol 35, Num 4, pp 617-624, issn 0001-1452Article

Experimental investigation of vortex dynamics on a 65° delta wing in sideslipGUGLIERI, G; QUAGLIOTTI, F. B.Aeronautical Journal. 1997, Vol 101, Num 1003, pp 111-120, issn 0001-9240Article

Generating parametrizations of wing geometries using partial differential equationsBLOOR, M. I. G; WILSON, M. J.Computer methods in applied mechanics and engineering. 1997, Vol 148, Num 1-2, pp 125-138, issn 0045-7825Article

Effects of leading-edge sweep angle on nonzero trimmed roll anglesSTEPHEN, E. J; SOPIRAK, D. A.Journal of aircraft. 1996, Vol 33, Num 4, pp 825-828, issn 0021-8669Conference Paper

Computation and visualization of the inviscid drag coefficient and polar surfaces of the wedged delta wing in supersonic flowNASTASE, A; HONERMANN, A.Zeitschrift für angewandte Mathematik und Mechanik. 1996, Vol 76, pp 629-630, issn 0044-2267, SUP2Conference Paper

Flow structure generated by oscillating delta-wing segmentsUTSCH, T; ROCKWELL, D.Journal of aircraft. 1990, Vol 27, Num 6, pp 574-576, issn 0021-8669, 3 p.Article

Seven hole probe measurement of leading edge vortex flowsPAYNE, F. M; NG, T. T; NELSON, R. C et al.Experiments in fluids. 1989, Vol 7, Num 1, pp 1-8, issn 0723-4864Article

Influence of the aspect ratio on the aerodynamics of the delta wing at high angle of attackZOHAR, Y; ER-EL, J.Journal of aircraft. 1988, Vol 25, Num 3, pp 200-205, issn 0021-8669Article

Shock-induced separated flows on the lee surface of delta wingsSESHADRI, S. N; NARAYAN, K. Y.Aeronautical Journal. 1987, Vol 91, Num 903, pp 128-141, issn 0001-9240Article

Effect of Slenderness Ratio on Free-to-Roll Wing AerodynamicsGRESHAM, N. T; WANG, Z; GURSUL, I et al.Journal of aircraft. 2011, Vol 48, Num 3, pp 1112-1116, issn 0021-8669, 5 p.Article

State-Space Modeling and Identification of Delta Wing Vortex-Coupled Roll DynamicsGORDON, Brandon W; PAKMEHR, Mehrdad; RABBATH, C. A et al.Journal of aircraft. 2009, Vol 46, Num 1, pp 36-45, issn 0021-8669, 10 p.Article

Experimental investigation of vortex flow over an 80 degree/60 degree double delta wing at sideslipATASHBAZ, G; OMMIAN, M.Journal of aircraft. 2006, Vol 43, Num 3, pp 840-843, issn 0021-8669, 4 p.Article

Experimental studies on control of delta wing aerodynamicsJINJUN WANG; YAN XU.AIAA journal. 2004, Vol 42, Num 2, pp 403-405, issn 0001-1452, 3 p.Article

Effects of Gurney flaps on the lift enhancement of a cropped nonslender delta wingLI, Y. C; WANG, J. J; TAN, G. K et al.Experiments in fluids. 2002, Vol 32, Num 1, pp 99-105, issn 0723-4864Article