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Performance and test section flow characteristics of the National Full-Scale Aerodynamics Complex 80- by 120-Foot Wind TunnelResults from the performance and test section flow calibration of the 80- by 120-Foot Wind Tunnel are presented. Measurements indicating the 80- by 120-ft test section flow quality were obtained throughout the tunnel operational envelope and for atmospheric wind speeds up to approximately 20 knots. Tunnel performance characteristics and a dynamic pressure system calibration were also documented during the process of mapping the test section flow field. Experimental results indicate that the test section flow quality is relatively insensitive to dynamic pressure and the level of atmospheric winds experienced during the calibration. The dynamic pressure variation in the test section is within +/-75 percent of the average. The axial turbulence intensity is less than 0.5 percent up to the maximum test section speed of 100 knots, and the vertical and lateral flow angle variations are within +/-5 deg and +/-7 deg, respectively. Atmospheric winds were found to affect the pressure distribution in the test section only at high ratios of wind speed to test section speed.
Document ID
19930014231
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Zell, Peter T.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-TM-103920
A-92058
NAS 1.15:103920
Report Number: NASA-TM-103920
Report Number: A-92058
Report Number: NAS 1.15:103920
Accession Number
93N23420
Funding Number(s)
PROJECT: RTOP 505-50-28
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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