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Methods for assessing wall interference in the 2- by 2-foot adaptive-wall wind tunnelDiscussed are two methods for assessing two-dimensional wall interference in the adaptive-wall test section of the NASA Ames 2 x 2-Foot Transonic Wind Tunnel: (1) a method for predicting free-air conditions near the walls of the test section (adaptive-wall methods); and (2) a method for estimating wall-induced velocities near the model (correction methods), both of which methods are based on measurements of either one or two components of flow velocity near the walls of the test section. Each method is demonstrated using simulated wind tunnel data and is compared with other methods of the same type. The two-component adaptive-wall and correction methods were found to be preferable to the corresponding one-component methods because: (1) they are more sensitive to, and give a more complete description of, wall interference; (2) they require measurements at fewer locations; (3) they can be used to establish free-stream conditions; and (4) they are independent of a description of the model and constants of integration.
Document ID
19870002367
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Schairer, E. T.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1986
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
A-86249
NASA-TM-88252
NAS 1.15:88252
Report Number: A-86249
Report Number: NASA-TM-88252
Report Number: NAS 1.15:88252
Accession Number
87N11800
Funding Number(s)
PROJECT: RTOP 505-65-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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