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File:Airfoil geometry.svg

Original file (SVG file, nominally 650 × 350 pixels, file size: 43 KB)

Description
English: an airfoil.
  • 1: zero lift line
  • 2: leading edge
  • 3: nose circle
  • 4: thickness
  • 5: camber
  • 6: upper surface
  • 7: trailing edge
  • 8: main camber line
  • 9: lower surface
Italiano: profilo alare.
  • 1: linea di portanza nulla
  • 2: bordo d'attacco
  • 3: cerchio osculatore del bordo d'attacco
  • 4: spessore
  • 5: curvatura
  • 6: dorso
  • 7: bordo d'uscita
  • 8: linea d'inarcamento media
  • 9: ventre
Date
Source McCormick, Aerodynamics of V/STOL flight, Dover Publications, ISBN 0486404609.
Author F l a n k e r
Permission
(Reusing this file)
Public domain This work has been released into the public domain by its author, F l a n k e r. This applies worldwide.

In some countries this may not be legally possible; if so:
F l a n k e r grants anyone the right to use this work for any purpose, without any conditions, unless such conditions are required by law.

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inception

3 November 2007

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image/svg+xml

checksum

8d9dac9d03e68b64de1103669f086279590d0a34

determination method or standard: SHA-1

data size

44,307 byte

height

350 pixel

width

650 pixel

File history

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Date/TimeThumbnailDimensionsUserComment
current20:13, 11 July 2016Thumbnail for version as of 20:13, 11 July 2016650 × 350 (43 KB)OttosfreundReverted to version as of 20:12, 11 July 2016 (UTC)
20:13, 11 July 2016Thumbnail for version as of 20:13, 11 July 2016650 × 350 (43 KB)OttosfreundReverted to version as of 11:43, 3 November 2007 (UTC)
20:12, 11 July 2016Thumbnail for version as of 20:12, 11 July 2016650 × 350 (43 KB)Ottosfreund3,5 changed, corrected
19:59, 11 July 2016Thumbnail for version as of 19:59, 11 July 2016650 × 350 (43 KB)Ottosfreund4 and 5 changed, corrected
11:43, 3 November 2007Thumbnail for version as of 11:43, 3 November 2007650 × 350 (43 KB)F l a n k e rAdded numbers
11:20, 3 November 2007Thumbnail for version as of 11:20, 3 November 2007650 × 350 (33 KB)F l a n k e r{{Information |Description={{en|an airfoil. *'''1''': zero lift line *'''2''': nose circle *'''3''': camber *'''4''': thickness}} {{it|profilo alare. *'''1''': linea di portanza nulla *'''2''': cerchio osculatore del bordo d'attacco *'''3''': curvatura *'

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