Wolfram|Alpha WidgetsOverviewTourGallerySign In

NACA Airfoil
Added Aug 1, 2010 by JeffreyBeckman in Engineering

Calculates parameters of a standard NACA airfoil including lift coefficient, center of pressure, pressure coefficients for both surfaces and a graphic representation of the flow field.

EMBED

Make your selections below, then copy and paste the code below into your HTML source.
* For personal use only.

Theme

Output Type






Output Width

px

Output Height

px
To add the widget to Blogger, click here and follow the easy directions provided by Blogger.
To add the widget to iGoogle, click here. On the next page click the "Add" button. You will then see the widget on your iGoogle account.
To embed this widget in a post on your WordPress blog, copy and paste the shortcode below into the HTML source:


For self-hosted WordPress blogs

To embed this widget in a post, install the Wolfram|Alpha Widget Shortcode Plugin and copy and paste the shortcode above into the HTML source.

To embed a widget in your blog's sidebar, install the Wolfram|Alpha Widget Sidebar Plugin, and copy and paste the Widget ID below into the "id" field:

To add a widget to a MediaWiki site, the wiki must have the Widgets Extension installed, as well as the code for the Wolfram|Alpha widget.

To include the widget in a wiki page, paste the code below into the page source.