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Investigation of some effects of humidity on aerodynamic characteristics on a 10-percent-thick NASA supercritical airfoilAn investigation was conducted in the Langley 8-foot transonic pressure tunnel to determine the effects of wind-tunnel humidity on the aerodynamic characteristics of a 10-percent-thick NASA supercritical airfoil. Effects of dewpoint variation from 267 K (20 F) to 294 K (70 F) were investigated. The tunnel stagnation temperature was 322 K (120 F) and the stagnation pressure was 0.1013 MN/09 m (1 atm).
Document ID
19830002748
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Jordan, F. L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1976
Subject Category
Aeronautics (General)
Report/Patent Number
L-10606
NASA-TM-X-3355
NAS 1.15:X-3355
Report Number: L-10606
Report Number: NASA-TM-X-3355
Report Number: NAS 1.15:X-3355
Accession Number
83N11018
Funding Number(s)
PROJECT: RTOP 505-06-31-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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