The effect of nacelle combinations and size on the zero-lift drag of a 45 degree sweptback wing and body configuration as determined by free-flight tests at Mach numbers between 0.8 and 1.3 (All Formats)

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

Read this report online.

Number of items: 24
Filetype: tif (image)

Download this report.

Number of items: 1
Filetype: pdf (file)