NASA Logo

NTRS

NTRS - NASA Technical Reports Server

The auto‑search feature has been disabled based on user feedback. Enter a search term/phrase and click “Search” to begin.

Back to Results
Devices Relaminarize Turbulent Flows On Swept WingsDrag reduced economically. Devices are small discontinuities built into surfaces of wings. Range from angled to straight, saw-toothed to square, and with and without concave steps. Saw-toothed configuration built into wings of future airplanes. Square devices machined separately and retrofitted to existing supersonic airplanes. Designed to reduce total airplane drag by changing high-drag turbulent wing-leading-edge flow to low-drag laminar wing-leading-edge flow. Used primarily on high-speed airplanes, but also useful in reducing drag in other applications.
Document ID
19940000572
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Creel, Theodore R.
(NASA Langley Research Center, Hampton, VA.)
Date Acquired
August 16, 2013
Publication Date
October 1, 1994
Publication Information
Publication: NASA Tech Briefs
Volume: 18
Issue: 10
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-14470
ISSN: 0145-319X
Report Number: LAR-14470
Accession Number
94B10572
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available