The Effect on Zero-Lift Drag of an Indented Fuselage or a Thickened Wing-Root Modification to a 45 Degree Sweptback Wing-Body Configuration as Determined by Flight Tests at Transonic Speeds (All Formats)

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

Read this report online.

Number of items: 22
Filetype: tif (image)

Download this report.

Number of items: 1
Filetype: pdf (file)