Read e-book online Aerodynamic Theory: A General Review of Progress Under a PDF

By William Frederick Durand

ISBN-10: 3642896308

ISBN-13: 9783642896309

ISBN-10: 364291487X

ISBN-13: 9783642914874

Dieser Buchtitel ist Teil des Digitalisierungsprojekts Springer ebook information mit Publikationen, die seit den Anfängen des Verlags von 1842 erschienen sind. Der Verlag stellt mit diesem Archiv Quellen für die historische wie auch die disziplingeschichtliche Forschung zur Verfügung, die jeweils im historischen Kontext betrachtet werden müssen. Dieser Titel erschien in der Zeit vor 1945 und wird daher in seiner zeittypischen politisch-ideologischen Ausrichtung vom Verlag nicht beworben.

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Extra info for Aerodynamic Theory: A General Review of Progress Under a Grant of the Guggenheim Fund for the Promotion of Aeronautics

Example text

The deviations from the potential flow involve only a minor correction of the theoretical value of the lift, whereas the drag depends entirely on the existence of these devia- Fig. 14. Ohange in the flow about tions. Since both phenomena, drag and a wing due to "dead-water" on one side: Above, potential flow: below, deviation of the actual from the theoflow with "dead-water". retical lift, can be reduced to the same cause, viz. deviations from the potential flow, it is to be assumed that a numerical relation connects the two.

422, 1932. J 1. GENERAL PROPERTIES OF THE WING 24 Figs. 21 and 22 show the distributions of pressure for two profiles with various angles of incidence 1. Figs. 23 and 24 show the two profiles with the points at which pressures were measured, and the polar curves thus obtained. 'The aspect ratio for these airfoils was 5. The values of the angle of incidence and resistance have not been recalculated for an infinite aspect ratio. 2 rt -0. 0. 0. 2 ~ Co. f87 o 91171113131{115 Figs. 23 and 24. Profiles 389 and 382 with points for pressure measure and the corresponding poiars.

Loco cit. Vol. 397, 1924. F. HOHNDORF, Verfahren zur Berechnung des Auftriebes gegebener Tragflachenprofile. loco cit. Vol. 265, 1926. , Theory of Wing Sections of Arbitrary Shape. S. A. Report No. 411, 1931. S. A. Reports Nos. 93, 124, 182, 244, 286, 315, Aerodynamic Characteristics of Airfoils (General Survey). Report 352, Large Scale Aerodynamic Characteristics of Airfoils as Tested in the Variable Density Wind Tunnel (General Survey). , Ergebnisse der Aerodynamischen Versuchsanstalt zu G6ttingen, Lief.

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Aerodynamic Theory: A General Review of Progress Under a Grant of the Guggenheim Fund for the Promotion of Aeronautics by William Frederick Durand


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