Skip to content

Home/Archive/NASA NTRS

NASA NTRS · 19930083213

Generalized conical-flow fields in supersonic wing theory

Lomax, Harvard·Heaslet, Max A

View original source ↗Export metadata ↓

Abstract

The source did not provide an abstract. Follow the original record for more information.

Explore related subjects

WINGS, COMPLETE - SWEEP FLOW, SUPERSONIC WINGS, COMPLETE - THEORY LOADS, STEADY - WINGS

Keep this discovery

Explore connections, maps & timelines

Lomax, Harvard, Heaslet, Max A. 1951-09-01. Generalized conical-flow fields in supersonic wing theory. https://ntrs.nasa.gov/citations/19930083213

Cite the original work for its findings. Save a collection to share your selection of sources.

KEEP EXPLORING

Related reports

NASA NTRS1951

Effect of Taper Ratio on the Low-speed Rolling Stability Derivatives of Swept and Unswept Wings of Aspect Ratio 2.61

Results of tests conducted in the 6-foot-diameter rolling-flow test section of the Langley stability tunnel to determine the effects of varying taper ratio on the rolling and static stability characteristics of a swept wing are presented; results are also given for the effects of varying taper ratio on an unswept wing and for the effects of sweep on a tapered wing. All the models were of aspect ratio 2.61 and had NACA 0012 sections normal to the quarter-chord line. Taper ratios of 1.00, 0.50, and 0.25 and sweep angles of 0 degrees and 45 degrees were investigated.

WINGS, COMPLETE - SWEEP↗