An Investigation of the Effects of Sweep on the Characteristics of a High-Aspect-Ratio Wing in the Langley 8-Foot High-Speed Tunnel by Richard T. Whitcomb
= An Investigation of the Effects of Sweep on the Characteristics of a High-Aspect-Ratio Wing in the Langley 8-Foot High-Speed Tunnel by Richard T. Whitcomb
{c}
{tag=Work by Richard T. Whitcomb}
{title2=1947}
{title2=NACA-RM-L6J01a}
https://ntrs.nasa.gov/citations/20030063954
NACA-RM-L6J01a,14 February 1947. Abstract: no sweep, ±30 degrees and ±45 degrees; Mach numbers 0.60–0.96; pressure measurements and wake surveys compare shock-associated changes.