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DE420325C - Device for the damping of vortices at the edge of aircraft wings u. like. - Google Patents

Device for the damping of vortices at the edge of aircraft wings u. like.

Info

Publication number
DE420325C
DE420325C DENDATM0083866 DEM0083866D DE420325C DE 420325 C DE420325 C DE 420325C DE NDATM0083866 DENDATM0083866 DE NDATM0083866 DE M0083866 D DEM0083866 D DE M0083866D DE 420325 C DE420325 C DE 420325C
Authority
DE
Grant status
Grant
Patent type
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
DENDATM0083866
Other languages
German (de)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CONSTANTIN MUSKALLA
Original Assignee
CONSTANTIN MUSKALLA
Publication date
Grant date

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16Blades
DENDATM0083866 Device for the damping of vortices at the edge of aircraft wings u. like. Expired DE420325C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DENDATM0083866 DE420325C (en) Device for the damping of vortices at the edge of aircraft wings u. like.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DENDATM0083866 DE420325C (en) Device for the damping of vortices at the edge of aircraft wings u. like.

Publications (1)

Publication Number Publication Date
DE420325C true DE420325C (en) 1925-10-19

Family

ID=7319737

Family Applications (1)

Application Number Title Priority Date Filing Date
DENDATM0083866 Expired DE420325C (en) Device for the damping of vortices at the edge of aircraft wings u. like.

Country Status (1)

Country Link
DE (1) DE420325C (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5088665A (en) * 1989-10-31 1992-02-18 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Serrated trailing edges for improving lift and drag characteristics of lifting surfaces
DE4208751A1 (en) * 1992-02-27 1993-11-11 Fritz Karl Hausser Reducing 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 (en) * 2005-11-15 2007-05-24 Airbus Deutschland Gmbh Braking 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
WO2007065434A1 (en) * 2005-12-05 2007-06-14 Lm Glasfiber A/S Blade for a wind turbine rotor
DE102006049616A1 (en) * 2006-10-20 2008-04-30 Deutsches 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

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5088665A (en) * 1989-10-31 1992-02-18 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Serrated trailing edges for improving lift and drag characteristics of lifting surfaces
DE4208751A1 (en) * 1992-02-27 1993-11-11 Fritz Karl Hausser Reducing 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 (en) * 2005-11-15 2007-05-24 Airbus Deutschland Gmbh Braking 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
WO2007065434A1 (en) * 2005-12-05 2007-06-14 Lm Glasfiber A/S Blade for a wind turbine rotor
DE102006049616A1 (en) * 2006-10-20 2008-04-30 Deutsches 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 (en) * 2006-10-20 2010-08-05 Deutsches Zentrum für Luft- und Raumfahrt e.V. Arrangement of an aerodynamic structure having a slotted rear or side edge in a flow

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