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

Proposed Boundary Conditions for Gust-Airfoil Interaction NoiseJAE WOOK KIM; LAU, Alex S. H; SANDHAM, Neil D et al.AIAA journal. 2010, Vol 48, Num 11, pp 2705-2710, issn 0001-1452, 6 p.Article

Aeroelastic Study of Bistable Composite AirfoilsDAYNES, S; WEAVER, P. M; POTTER, K. D et al.Journal of aircraft. 2009, Vol 46, Num 6, pp 2169-2174, issn 0021-8669, 6 p.Article

Flow over an airfoil with jetsKRASSIN, Y. A.Journal of aircraft. 1989, Vol 26, Num 3, pp 241-246, issn 0021-8669Article

Design of airfoils and cascades of airfoilsKORAKIANITIS, T. P.AIAA journal. 1989, Vol 27, Num 4, pp 455-461, issn 0001-1452, 7 p.Article

Wing-section effects on the flight performance of a remotely piloted vehiclesSTOLLERY, J. L; DYER, D. J.Journal of aircraft. 1989, Vol 26, Num 10, pp 932-938, issn 0021-8669, 7 p.Conference Paper

On the prospects for increasing dynamic liftMABEY, D. G.Aeronautical Journal. 1988, Vol 92, Num 913, pp 95-106, issn 0001-9240Article

Thick airfoil at low Reynolds number and high incidenceRAGHUNATHAN, S; HARRISON, J. R; HAWKINS, B. D et al.Journal of aircraft. 1988, Vol 25, Num 7, pp 669-671, issn 0021-8669Article

Extension of inverse design techniques for multicomponent airfoilsSILADIC, M; CAREY, G. F.AIAA journal. 1988, Vol 26, Num 6, pp 745-747, issn 0001-1452Article

A combination conformal-transfinite mapping method for grids about fin-afterbody combinationsHOFFMAN, G. H.Applied mathematics and computation. 1987, Vol 22, Num 4, pp 309-331, issn 0096-3003Article

A correlation between aerofoil theory and Euler's equation for calculating the head of a constant-pitch axial-flow inducerYEDIDIAH, S.Proceedings of the Institution of Mechanical Engineers. Part C. Mechanical engineering science. 1987, Vol 201, Num 5, pp 357-363, issn 0263-7154Article

Newtonian theory for the compression surface of airfoils at moderate or large incidenceHEMDAN, H. T.AIAA journal. 1987, Vol 25, Num 10, pp 1281-1285, issn 0001-1452Article

A thick symmetrical aerofoil oscillating about zero incidence angleRAGHUNATHAN, S; OMBAKA, O. O.International journal of heat and fluid flow. 1986, Vol 7, Num 2, pp 155-159, issn 0142-727XArticle

Cita, la voie du carénage = Cita, the way of careenageSystèmes solaires (Revue). 2001, Num 143, pp 58-59, issn 0295-5873Article

Aerodynamics of human=powered flightDRELA, M.Annual review of fluid mechanics. 1990, Vol 22, pp 93-110, issn 0066-4189, 18 p.Article

Correlation of lift and thickness noise sources in vortex-airfoil interactionHOWE, M. S.Journal of sound and vibration. 1990, Vol 137, Num 1, pp 1-7, issn 0022-460XArticle

Method for calculating the unsteady flow of an elliptical circulation-control airfoilMAO SUN; WEI WANG.Journal of aircraft. 1989, Vol 26, Num 10, pp 907-913, issn 0021-8669, 7 p.Article

On unsteady airfoil-vortex interactionNAKAGAWA, T.Acta mechanica. 1988, Vol 75, Num 1-4, pp 1-13, issn 0001-5970Article

Propulsive vortical signature for plunging and pitching airfoilsFREYMUTH, P.AIAA journal. 1988, Vol 26, Num 7, pp 881-883, issn 0001-1452Article

Synthesis and analysis of flow about airfoils with interactive graphicsRASHEED, S. M; AL-HASHEMY, R. K; SHEIKH AHMAD, A. I et al.Computers & graphics. 1988, Vol 12, Num 1, pp 99-110, issn 0097-8493Article

Supersonic airfoil optimizationPITTMAN, J. L.Journal of aircraft. 1987, Vol 24, Num 12, pp 873-879, issn 0021-8669Article

Radial transport and momentum exchange in an axial compressorDRING, R. P.Journal of turbomachinery. 1993, Vol 115, Num 3, pp 477-486, issn 0889-504XConference Paper

Computational methods for aerodynamic deisgn (inverse) and optimization, Loen, Norway, 22-23 May 1989AGARD conference proceedings. 1990, Num 463, issn 0549-7191, 354 p.Conference Proceedings

Separated flows developing under increasingly adverse pressure gradientsMEHTA, J. M.Journal of aircraft. 1989, Vol 26, Num 1, pp 91-93, issn 0021-8669Article