Free-Flight Investigation of Fullspan, 0.2 Chord Plain Ailerons at High Subsonic, Transonic, and Supersonic Speeds to Determine Some Effects of Wing Sweepback, Taper, Aspect Ratio, and Section-Thickness Ratio (All Formats)
This item is available in multiple formats. Choose one below.
Number of items: | 21 |
---|---|
Filetype: | tif (image) |
Number of items: | 1 |
---|---|
Filetype: | pdf (file) |