Results of Rocket Model Test of an Airplane Configuration Having an Arrow Wing and Slender Flat-Sided Fuselage: Lift, Drag, Longitudinal Stability, Lateral Force, and Jet Effects at Mach Numbers Between 1.0 and 2.3 (All Formats)

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

Read this report online.

Number of items: 28
Filetype: tif (image)

Download this report.

Number of items: 1
Filetype: pdf (file)