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Numerical simulation of thin airfoil stall by using a modified DES approachDONG LI.International journal for numerical methods in fluids. 2007, Vol 54, Num 3, pp 325-332, issn 0271-2091, 8 p.Article

Fluid forces on a very low Reynolds number airfoil and their predictionZHOU, Y; MD. MAHBUB ALAM; YANG, Hx et al.International journal of heat and fluid flow. 2011, Vol 32, Num 1, pp 329-339, issn 0142-727X, 11 p.Article

Comments on the paper Chaotic motions of a two-dimensional airfoil with cubic nonlinearity in supersonic flowALGABA, Antonio; FERNANDEZ-SANCHEZ, Fernando; MERINO, Manuel et al.Aerospace science and technology (Imprimé). 2013, Vol 28, Num 1, pp 431-434, issn 1270-9638, 4 p.Article

Design of high-efficiency turbomachinery blades for energy conversion devices with the three-dimensional prescribed surface curvature distribution blade design (CIRCLE) methodKORAKIANITIS, T; HAMAKHAN, I. A; REZAIENIA, M. A et al.Applied energy. 2012, Vol 89, Num 1, pp 215-227, issn 0306-2619, 13 p.Article

Neural networks based airfoil generation for a given Cp using Bezier―PARSEC parameterizationKHARAL, Athar; SALEEM, Ayman.Aerospace science and technology (Imprimé). 2012, Vol 23, Num 1, pp 330-344, issn 1270-9638, 15 p.Article

Design of a new urban wind turbine airfoil using a pressure-load inverse methodHENRIQUES, J. C. C; MARQUES DA SILVA, F; ESTANQUEIRO, A. I et al.Renewable energy. 2009, Vol 34, Num 12, pp 2728-2734, issn 0960-1481, 7 p.Article

Unsteady thin airfoil theory revisited for a general deforming airfoilJOHNSTON, Christopher O; MASON, William H; HAN, Cheolheui et al.Journal of mechanical science and technology. 2010, Vol 24, Num 12, pp 2451-2460, issn 1738-494X, 10 p.Article

Vortex structure and scale on an unsteady airfoilFUCHIWAKI, Masaki; TANAKA, Kazuhiro.JSME international journal. Series B, fluids and thermal engineering. 2006, Vol 49, Num 4, pp 1056-1063, issn 1340-8054, 8 p.Conference Paper

AERODYNAMIC CHARACTERISTICS OF AIRFOILS WITH ENERGY SUPPLYAULCHENKO, S. M; ZAMURAEV, V. P; KALININA, A. P et al.Journal of applied mechanics and technical physics. 2009, Vol 50, Num 5, pp 760-767, issn 0021-8944, 8 p.Article

DESIGN OF A TWO-ELEMENT AIRFOIL IN A RANGE OF ANGLES OF ATTACKABZALILOV, D. F.Journal of applied mechanics and technical physics. 2008, Vol 49, Num 6, pp 978-984, issn 0021-8944, 7 p.Article

Aerodynamic analysis of the boundary layer region of symmetric airfoils at ground proximityGHADIMI, Parviz; ALI BAKHSHANDEH ROSTAMI; JAFARKAZEMI, Farzad et al.Aerospace science and technology (Imprimé). 2012, Vol 17, Num 1, pp 7-20, issn 1270-9638, 14 p.Article

A correlation indicating incipient dynamic stallGRACEY, M. W; NIVEN, A. J; COTON, F. N et al.Aeronautical Journal. 1996, Vol 100, Num 997, pp 305-311, issn 0001-9240Article

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

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

Numerical modeling of an S809 airfoil under dynamic stall, erosion and high reduced frequenciesGHARALI, Kobra; JOHNSON, David A.Applied energy. 2012, Vol 93, pp 45-52, issn 0306-2619, 8 p.Conference Paper

Motion of an airfoil near a flat screenGORELOV, D. N; GORLOV, S. I.Journal of applied mechanics and technical physics. 1995, Vol 36, Num 1, pp 45-49, issn 0021-8944Article

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

Drag reduction due to riblets on a GAW(2) airfoilSUBASCHANDAR, N; KUMAR, R; SUNDARAM, S et al.Journal of aircraft. 1999, Vol 36, Num 5, pp 890-892, issn 0021-8669Article

Supersonic indicial lift functions from transform methodsJAWORSKI, Justin W; DOWELL, Earl H.AIAA journal. 2007, Vol 45, Num 8, pp 2106-2111, issn 0001-1452, 6 p.Article

Derivation of four-digit airfoils from the Sunya airfoilRAMAMOORTHY, P.Journal of aircraft. 1997, Vol 34, Num 3, pp 441-443, issn 0021-8669Article

Sur les mécanismes de couplage écoulement-structure = On the flow-structure coupling mechanismsDAT, R.R.F.M. Revue française de mécanique. 1995, Num 1, pp 13-22, issn 0373-6601Article

Finite state aeroelastic model for use in rotor design optimizationCHENGJIAN HE; PETERS, D. A.Journal of aircraft. 1993, Vol 30, Num 5, pp 777-784, issn 0021-8669Article

Note on Parameterization of AirfoilsYOUNG, D. P.AIAA journal. 2011, Vol 49, Num 1, pp 254-255, issn 0001-1452, 2 p.Article

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