On linearized airfoil and bluff-body stability theory and the Scruton numberSCANLAN, R. H.Journal of wind engineering and industrial aerodynamics. 1983, Vol 12, Num 3, pp 373-378, issn 0167-6105Article

Minimum induced drag of wings with curved planformASHENBERG, J; WEIHS, D.Journal of aircraft. 1984, Vol 21, Num 1, pp 89-91, issn 0021-8669Article

Airfoil optimizationKRANTZ, P; HEDMAN, S. G.Journal of aircraft. 1986, Vol 23, Num 5, pp 355-356, issn 0021-8669Article

ETUDE D'UN SYSTEME PROPULSIFCOUCHET G.1981; J. MEC.; ISSN 0021-7832; FRA; DA. 1981; VOL. 20; NO 1; PP. 169-178; ABS. ENG; BIBL. 5 REF.Article

SUR LES PROFILS AERODYNAMIQUES.COUCHET G; LAPORTE R.1975; J. MEC.; FR.; DA. 1975; VOL. 14; NO 3; PP. 523-530; ABS. ANGL.; BIBL. 7 REF.Article

Tail load calculations for light airplanesLAITONE, E. V.Journal of aircraft. 1994, Vol 31, Num 2, pp 466-469, issn 0021-8669Article

Unsteady transonic flow calculations for interfering lifting surface configurationsBATINA, J. T.Journal of aircraft. 1986, Vol 23, Num 5, pp 422-430, issn 0021-8669Article

Transient aerodynamic characteristics of a two-dimensional airfoil during stepwise incidence variationAIHARA, Y; KOYAMA, H; MURASHIGE, A et al.Journal of aircraft. 1985, Vol 22, Num 8, pp 661-668, issn 0021-8669Article

A general iterative method to design Kármán-Trefftz and Joukowsky airfoilsYUKSELEN, M. A; ERIM, M. Z.International journal for numerical methods in engineering. 1984, Vol 20, Num 7, pp 1349-1368, issn 0029-5981Article

High-lift airfoil design from the hodographCOHEN, M. J.Journal of aircraft. 1984, Vol 21, Num 10, pp 760-766, issn 0021-8669Article

Laser holographic interferometry for an unsteady airfoil undergoing dynamic stallLEE, G; BUELL, D. A; LICURSI, J. P et al.AIAA journal. 1984, Vol 22, Num 4, pp 504-511, issn 0001-1452Article

Exemple d'écoulement de gaz sonique autour d'un profil asymétriqueLICHUK, S. T; OREL, A. A.Prikladnaâ mehanika i tehničeskaâ fizika. 1984, Num 5, pp 76-81, issn 0869-5032Article

Hodograph method for airfoil design : The general caseLIMACHE, A. C.Journal of aircraft. 1996, Vol 33, Num 4, pp 680-690, issn 0021-8669Article

Multipoint inverse airfoil design method for slot-suction airfoilsSAEED, F; SELIG, M. S.Journal of aircraft. 1996, Vol 33, Num 4, pp 708-715, issn 0021-8669Conference Paper

Steady and unsteady transonic pressure distributions on NACA 0012TRIEBSTEIN, H.Journal of aircraft. 1986, Vol 23, Num 3, pp 213-219, issn 0021-8669Article

A new fast solver procedure applied to the BGK computer program for transonic flow past on airfoilYAU SHU WONG; JONES, D. J.Canadian aeronautics and space journal. 1985, Vol 31, Num 2, pp 159-169, issn 0008-2821Article

Evaluation of a stalled airfoil analysis programRUMSEY, C. L.Journal of aircraft. 1985, Vol 22, Num 2, pp 156-157, issn 0021-8669Article

Transonic time responses of the MBB A-3 supercritical airfoil including active controlsBATINA, J. T; YANG, T. Y.Journal of aircraft. 1985, Vol 22, Num 5, pp 393-400, issn 0021-8669Article

The aerodynamic characteristics of a GU25-5(11) 8 aerofoil for low Reynolds numbersGALBRAITH, R. A. M.Experiments in fluids. 1985, Vol 3, Num 5, pp 253-256, issn 0723-4864Article

Aerodynamic coefficients and longitudinal stability of sail aerofoilsSNEYD, A. D.Journal of Fluid Mechanics. 1984, Vol 149, pp 127-146, issn 0022-1120Article

Experimental investigation of vortex breakdown over a sideslipping canard-configurated aircraft modelHEBBAR, S. K; PLATZER, M. F; CHANG HO KIM et al.Journal of aircraft. 1994, Vol 31, Num 4, pp 998-1001, issn 0021-8669Article

Supersonic transport wing minimum weight design integrating aerodynamics and structuresBARTHELEMY, J.-F. M; WRENN, G. A; DOVI, A. R et al.Journal of aircraft. 1994, Vol 31, Num 2, pp 330-338, issn 0021-8669Conference Paper

The vortex roll-up problem using lamb vortices for the elliptically loaded wingDALTON, C; XUEGENG WANG.Computers & fluids. 1990, Vol 18, Num 1, pp 139-150, issn 0045-7930, 12 p.Article

Investigation of internal singularity method for multielement airfoilsCHEN, D. R; SHEU, M. J.Journal of aircraft. 1989, Vol 26, Num 2, pp 189-192, issn 0021-8669Article

A class of airfoils having finite trailing-edge pressure gradientsORMSBEE, A. I; MAUGHMER, M. D.Journal of aircraft. 1986, Vol 23, Num 2, pp 97-103, issn 0021-8669Article