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Publication numberDE420325 C
Publication typeGrant
Application numberDENDATM0083866
Publication date19 Oct 1925
Publication numberDE 420325 C, DE 420325C, DE-C-420325, DE420325 C, DE420325C, DENDATM0083866
ApplicantConstantin Muskalla
Export CitationBiBTeX, EndNote, RefMan
External Links: DPMA, Espacenet
Vorrichtung zur Daempfung von Randwirbeln an Flugzeug-Tragflaechen u. dgl. Apparatus for Damping of edge vortices on aircraft wings and. Like. translated from German
DE 420325 C
Abstract  available in
Description  available in
Claims  available in
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
DE4208751A1 *20 Mar 199211 Nov 1993Fritz Karl HausserReducing resistance to aerofoil or hydrofoil passing through medium e.g. air or water - uses array of teeth formed on leading and/or trailing edge of aerofoil or hydrofoil section
DE102005054248A1 *15 Nov 200524 May 2007Airbus Deutschland GmbhBraking flap for deceleration of aircraft against air-flow which surrounds aircraft, comprises many vortex edges, which resolve individual edge section into number of vortex part, are arranged at free edge
DE102006049616A1 *20 Oct 200630 Apr 2008Deutsches Zentrum für Luft- und Raumfahrt e.V.Aerodynamic component has slits at the trailing edge, running between the upper and lower main surfaces, to reduce air turbulence noise emissions
DE102006049616B4 *20 Oct 20065 Aug 2010Deutsches Zentrum für Luft- und Raumfahrt e.V.Anordnung eines Aerodynamischen Bauteils mit einer geschlitzten Hinter- oder Seitenkante in einer Strömung
US5088665 *31 Oct 198918 Feb 1992The United States Of America As Represented By The Administrator Of The National Aeronautics And Space AdministrationSerrated trailing edges for improving lift and drag characteristics of lifting surfaces
WO2007065434A1 *5 Dec 200614 Jun 2007Lm Glasfiber A/SBlade for a wind turbine rotor
International ClassificationB64C11/16
Cooperative ClassificationB64C11/16
European ClassificationB64C11/16