Low-speed experimental determination of the effects of leading-edge radius and profile thickness on static and oscillatory lateral stability derivatives for a delta wing with 60 degrees of leading-edge sweep (All Formats)

This item is available in multiple formats. Choose one below.

Read this report online.

Number of items: 46
Filetype: tif (image)

Download this report.

Number of items: 1
Filetype: pdf (file)