File:Airfoil thickness definition.svg

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Summary

Two different and incompatible definitions of <a href="https://en.wikipedia.org/wiki/Airfoil" class="extiw" title="en:Airfoil">airfoil</a> thickness are used in the aerodynamics field (here illustrated on the same airfoil).

  • In case A above the thickness is measured perpendicular to the foil camber line. This is sometimes described as the "American convention"<a href="#cite_note-Houghton-1">[1]</a> and can be seen in Houghton & Carpenter 2003,<a href="#cite_note-Houghton-1">[1]</a> Phillips 2010.<a href="#cite_note-2">[2]</a>
  • In case B above the thickness is measured perpendicular to the foil chord line. This is sometimes described as the "British convention" and can be seen in Bertin & Cummings 2009<a href="#cite_note-3">[3]</a>.

Note that each definition implies a different camber line geometry for a given airfoil. Since the camber line curvature is small on most aircraft, the effect of difference between the definitions is often small.

  1. ↑ <a href="#cite_ref-Houghton_1-0">a</a> <a href="#cite_ref-Houghton_1-1">b</a> Houghton, E. L.; Carpenter, P.W. () Butterworth Heinmann , ed. Aerodynamics for Engineering Students (5th ed.) <a href="https://en.wikipedia.org/wiki/International_Standard_Book_Number" class="extiw" title="en:International Standard Book Number">ISBN</a>: <a href="//commons.wikimedia.org/wiki/Special:BookSources/0750651113" title="Special:BookSources/0750651113">0750651113</a>. p.17
  2. <a href="#cite_ref-2">↑</a> Phillips, Warren F. () Mechanics of Flight (2nd ed.), Wiley & Sons <a href="https://en.wikipedia.org/wiki/International_Standard_Book_Number" class="extiw" title="en:International Standard Book Number">ISBN</a>: <a href="//commons.wikimedia.org/wiki/Special:BookSources/9780470539750" title="Special:BookSources/9780470539750">9780470539750</a>. p.27
  3. <a href="#cite_ref-3">↑</a> Bertin, John J.; Cummings, Russel M. () Pearson Prentice Hall , ed. Aerodynamics for Engineers (5th ed.) <a href="https://en.wikipedia.org/wiki/International_Standard_Book_Number" class="extiw" title="en:International Standard Book Number">ISBN</a>: <a href="//commons.wikimedia.org/wiki/Special:BookSources/9780132272681" title="Special:BookSources/9780132272681">9780132272681</a>. p.199

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File history

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Date/TimeThumbnailDimensionsUserComment
current01:03, 5 January 2017Thumbnail for version as of 01:03, 5 January 2017672 × 593 (29 KB)127.0.0.1 (talk)Two different and incompatible definitions of <a href="https://en.wikipedia.org/wiki/Airfoil" class="extiw" title="en:Airfoil">airfoil</a> thickness are used in the aerodynamics field (here illustrated on the same airfoil). <ul><li> In <b>case A</b> above the thickness is measured <i>perpendicular to the foil camber line</i>. This is sometimes described as the "American convention"<sup id="cite_ref-Houghton_1-0" class="reference"><a href="#cite_note-Houghton-1">[1]</a></sup> and can be seen in Houghton & Carpenter 2003,<sup id="cite_ref-Houghton_1-1" class="reference"><a href="#cite_note-Houghton-1">[1]</a></sup> Phillips 2010.<sup id="cite_ref-2" class="reference"><a href="#cite_note-2">[2]</a></sup> </li></ul> <ul><li> In <b>case B</b> above the thickness is measured <i>perpendicular to the foil chord line</i>. This is sometimes described as the "British convention" and can be seen in Bertin & Cummings 2009<sup id="cite_ref-3" class="reference"><a href="#cite_note-3">[3]</a></sup>.</li></ul> <p>Note that each definition implies a different camber line geometry for a given airfoil. Since the camber line curvature is small on most aircraft, the effect of difference between the definitions is often small. </p> <ol class="references"> <li id="cite_note-Houghton-1"> <span class="mw-cite-backlink">↑ <a href="#cite_ref-Houghton_1-0"><sup><i><b>a</b></i></sup></a> <a href="#cite_ref-Houghton_1-1"><sup><i><b>b</b></i></sup></a></span> <span class="reference-text"><cite class="book" style="font-style:normal">Houghton, E. L.; Carpenter, P.W. (<span style="white-space:nowrap"><time class="dtstart" datetime="2003">2003</time></span>) Butterworth Heinmann , ed. <i> Aerodynamics for Engineering Students</i> (5<sup>th</sup> ed.) <small><a href="https://en.wikipedia.org/wiki/International_Standard_Book_Number" class="extiw" title="en:International Standard Book Number">ISBN</a>: <a href="//commons.wikimedia.org/wiki/Special:BookSources/0750651113" title="Special:BookSources/0750651113">0750651113</a>. </small></cite> p.17</span> </li> <li id="cite_note-2"> <span class="mw-cite-backlink"><a href="#cite_ref-2">↑</a></span> <span class="reference-text"><cite class="book" style="font-style:normal">Phillips, Warren F. (<span style="white-space:nowrap"><time class="dtstart" datetime="2010">2010</time></span>) <i> Mechanics of Flight</i> (2<sup>nd</sup> ed.), Wiley & Sons <small><a href="https://en.wikipedia.org/wiki/International_Standard_Book_Number" class="extiw" title="en:International Standard Book Number">ISBN</a>: <a href="//commons.wikimedia.org/wiki/Special:BookSources/9780470539750" title="Special:BookSources/9780470539750">9780470539750</a>. </small></cite> p.27</span> </li> <li id="cite_note-3"> <span class="mw-cite-backlink"><a href="#cite_ref-3">↑</a></span> <span class="reference-text"><cite class="book" style="font-style:normal">Bertin, John J.; Cummings, Russel M. (<span style="white-space:nowrap"><time class="dtstart" datetime="2009">2009</time></span>) Pearson Prentice Hall , ed. <i> Aerodynamics for Engineers</i> (5<sup>th</sup> ed.) <small><a href="https://en.wikipedia.org/wiki/International_Standard_Book_Number" class="extiw" title="en:International Standard Book Number">ISBN</a>: <a href="//commons.wikimedia.org/wiki/Special:BookSources/9780132272681" title="Special:BookSources/9780132272681">9780132272681</a>. </small></cite> p.199</span> </li> </ol>
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