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Adaptive wall testing sections (AWTS)The lecture starts with conventional techniques of minimizing wall interference and explains the principle of wall streamlining. The history of AWTS development is highlighted, along with the benefits of wall streamlining, including minimized boundary interference, increased model size, reduced tunnel drive power, noise, and volume, as well as multiple flow field simulations to be performed using one test section. AWTS-associated problems coming from the need to adjust the test-section boundaries for each test condition are assessed, along with the requirements of a boundary-adjustment strategy. Examples of two- and three-dimensional test sections are presented, and attention is focused on residual interference and the effects of compressibility and model lift on flexible-wall contours.
Document ID
19910032946
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wolf, Stephen W. D.
(NASA Langley Research Center Hampton, VA, United States)
Kilgore, Robert A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
October 1, 1987
Subject Category
Research And Support Facilities (Air)
Accession Number
91A17569
Distribution Limits
Public
Copyright
Other

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