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Additional flow quality measurements in the Langley Research Center 8-Foot Transonic Pressure TunnelAdditional tests were conducted to further define the disturbance characteristics of the Langley 8-Foot Transonic Pressure Tunnel. Measurements were made in the settling chamber with hot wire probes and in the test section with pressure transducers when various methods were used to choke the flow. In addition to presenting rms values measured at various locations and tunnel condition, autocorrelations and cross correlation data are also presented.
Document ID
19800042774
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Brooks, J. D.
(NASA Langley Research Center Hampton, VA, United States)
Stainback, P. C.
(NASA Langley Research Center Hampton, VA, United States)
Brooks, C. W., Jr.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 80-0434
Meeting Information
Meeting: Aerodynamic Testing Conference
Location: Colorado Springs, CO
Start Date: March 18, 1980
End Date: March 20, 1980
Accession Number
80A26944
Distribution Limits
Public
Copyright
Other

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