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Wind tunnel results of the high-speed NLF(1)-0213 airfoilWind tunnel tests were conducted to evaluate a natural laminar flow airfoil designed for the high speed jet aircraft in general aviation. The airfoil, designated as the High Speed Natural Laminar Flow (HSNLF)(1)-0213, was tested in two dimensional wind tunnels to investigate the performance of the basic airfoil shape. A three dimensional wing designed with this airfoil and a high lift flap system is also being evaluated with a full size, half span model.
Document ID
19900003226
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sewall, William G. (NASA Langley Research Center Hampton, VA, United States)
Mcghee, Robert J. (NASA Langley Research Center Hampton, VA, United States)
Hahne, David E. (NASA Langley Research Center Hampton, VA, United States)
Jordan, Frank L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1987
Publication Information
Publication: Research in Natural Laminar Flow and Laminar-Flow Control, Part 3
Subject Category
Aerodynamics
Accession Number
90N12542
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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