 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

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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 by

Codex  0 2026-11-05

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.

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