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Description and calibration of the Langley unitary plan wind tunnelThe two test sections of the Langley Unitary Plan Wind Tunnel were calibrated over the operating Mach number range from 1.47 to 4.63. The results of the calibration are presented along with a a description of the facility and its operational capability. The calibrations include Mach number and flow angularity distributions in both test sections at selected Mach numbers and tunnel stagnation pressures. Calibration data are also presented on turbulence, test-section boundary layer characteristics, moisture effects, blockage, and stagnation-temperature distributions. The facility is described in detail including dimensions and capacities where appropriate, and example of special test capabilities are presented. The operating parameters are fully defined and the power consumption characteristics are discussed.
Document ID
19820004162
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Jackson, C. M., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Corlett, W. A.
(NASA Langley Research Center Hampton, VA, United States)
Monta, W. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1981
Subject Category
Aerodynamics
Report/Patent Number
L-14024
NASA-TP-1905
Report Number: L-14024
Report Number: NASA-TP-1905
Accession Number
82N12035
Funding Number(s)
PROJECT: RTOP 505-42-23-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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