Portal de Periódicos da CAPES

THE DESIGN AND APPLICATION OF HIGH LIFT DEVICES

1968; Wiley; Volume: 154; Issue: 2 Linguagem: Inglês

10.1111/j.1749-6632.1968.tb15206.x

1749-6632

J. C. Wimpenny,

Aerospace and Aviation Technology

Annals of the New York Academy of SciencesVolume 154, Issue 2 p. 329-366 THE DESIGN AND APPLICATION OF HIGH LIFT DEVICES J. C. Wimpenny, J. C. Wimpenny Hawker Siddeley Aviation Limited Hatfield, Herts, EnglandSearch for more papers by this author J. C. Wimpenny, J. C. Wimpenny Hawker Siddeley Aviation Limited Hatfield, Herts, EnglandSearch for more papers by this author First published: November 1968 https://doi.org/10.1111/j.1749-6632.1968.tb15206.xCitations: 4AboutPDF ToolsRequest permissionExport citationAdd to favoritesTrack citation ShareShare Give accessShare full text accessShare full-text accessPlease review our Terms and Conditions of Use and check box below to share full-text version of article.I have read and accept the Wiley Online Library Terms and Conditions of UseShareable LinkUse the link below to share a full-text version of this article with your friends and colleagues. Learn more.Copy URL Share a linkShare onEmailFacebookTwitterLinkedInRedditWechat REFERENCES 1 ABBOTT, I. H. & A. E. VON DOENHOFF. 1958. Theory of Wing Sections. Dover Publications Inc. New York , N.Y. 2 THEODORSON, T. 1931. On the theory of wing sections with particular reference to the lift distribution. NACA TR 383. Nat. Adv. Comm. Aero., Washington, D.C. 3 HAY, J. A. & W. J. EGGINGTON. 1956. An exact theory of a thin aerofoil with large flap deflection. J. Roy. Aero. Soc. 60(551): 753–757. 4 HILL, P. G. U. W. SCHAUB & Y. SENOO. 1963. Turbulent wakes in pressure gradients. TRANS. A.S.M.E. Series E. J. Appl. Mech. 30(4): 518–524. 5 WILKINSON, D. H. 1965. Predictions of the lift, drag and air requirements for an aircraft with a blown flap. Aero. Dept. Rept. 5416/DHW/FM. Hawker Siddeley Aviation Ltd., Hatfield, England. 6 HARPER, C. W. & R. L. MAKI. 1964. A review of the stall characteristics of swept wings. NASA TN D-2373. Washington, D.C. 7 STRATFORD, B. S. 1959. Prediction of separation of turbulent boundary layer, and an experimental flow with zero skin friction throughout its region of pressure rise. J. Fluid Mech. 5(1). 8 BISHOP, G. E. G. 1966. Fluid motion programme, F03A (method two). D. H. MATHS. Rept. 329/GBD/F03A. Hawker Siddeley Aviation Ltd., Hatfield , England . 9 CONE, C. D. The theory of induced lift and minimum induced drag of non-planar lifting systems. NASA TRR-139. Washington, D.C. 10 ANDERSON, S. B., H. C. QUIGLEY & R. C. INNIS. 1965. Stability and control considerations for S.T.O.L. aircraft. AGARD Rept. 504. NATO. Paris , France . 11 FINK, M. P. 1961. Aerodynamic characteristics, temperature and noise measurements of a large scale external-flow jet-augmented-flap model with turbojet engines operating. NASA TN D-943. Washington, D.C. Citing Literature Volume154, Issue2International Congress on Subsonic AeronauticsNovember 1968Pages 329-366 ReferencesRelatedInformation