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File:Gurney flap (NASA technical memorandum).png
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Summary

DescriptionGurney flap (NASA technical memorandum).png
English: Title: A water tunnel study of Gurney flaps.


Abstract: "Several Gurney flap configurations were tested in the——NASA Langley 16 x 24 inch Water Tunnel. These devices provided an increased region of attached flow on a wing upper surface relative——to the "wing without the flaps." The recirculation region behind the flap was visualized. And shown——to be, "consistent with hypotheses stated in previous research." Although the test Reynolds number for this study was several orders of magnitude below those in previous investigations, "the effect of the Gurney flaps is in qualitative agreement with them." This is as would be expected from first order effects for high lift devices."
Date
Source From Figure-1 in NASA Technical Memorandum 4071, which itself quotes Liebeck, Robert H.: Design of Subsonic Airfoils for High Lift. Journal of Aircraft, vol. 15, no. 9, Sept. 1978, pp. 547-561.
Author

Neuhart, Dan H.; Pendergraft, Odis C., Jr. at Langley Research Center (NASA document)

Liebeck, Robert H (figure drawing).

Licensing

Public domainPublic domainfalsefalse
Public domain This image of simple geometry is ineligible for copyright and therefore in the public domain, because it consists entirely of information that is common property and "contains no original authorship."
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Transferred from en.wikipedia to Commons by, Ariadacapo using CommonsHelper.

The original description page was here. All following user names refer to en.wikipedia.
  • 2007-07-06 02:45 Dhaluza 724×236× (10117 bytes) From Figure-1 in ※ Title: *A water tunnel study of Gurney flaps Author(s): *Neuhart, Dan H.; Pendergraft, Odis C., Jr. Abstract: *Several
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Newman airfoil

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September 1978

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Date/TimeThumbnailDimensionsUserComment
current06:15, 28 August 2012Thumbnail for version as of 06:15, 28 August 2012724 × 236 (10 KB)File Upload Bot (Magnus Manske)Transfered from en.wikipedia by User:Ariadacapo using CommonsHelper

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