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Adaptive wall technology for minimization of wind tunnel boundary interferences - where are we now?The status of adaptive wall technology to improve wind tunnel simulations for 2- and 3-D testing is reviewed. This technology relies on the test section flow boundaries being adjustable, using a tunnel/computer system to control the boundary shapes without knowledge of the model under test. This paper briefly overviews the benefits and shortcomings of adaptive wall testing techniques. A historical perspective highlights the disjointed development of these testing techniques from 1938 to present. Currently operational transonic Adaptive Wall Test Sections (AWTSs) are detailed, showing a preference for the simplest AWTS design with two solid flexible walls. Research highlights show that quick wall adjustment procedures are available and AWTSs, with impervious or ventilated walls, can be used through the transonic range up to M(sub infinity) = 1.2. The requirements for production testing in AWTSs are discussed, and conclusions drawn as to the current status of adaptive wall technology. In 2-D testing, adaptive wall technology is mature enough for general use, even in cryogenic wind tunnels. In 3-D testing, this technology has not been pursued aggressively, because of the inertia against change in testing techniques, and preconceptions about the difficulties of using AWTSs.
Document ID
19950057304
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wolf, Stephen W. D.
(NASA Ames, Moffett Field, CA US, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1994
Publication Information
Publisher: World Scientific Pub. Co. Pte. Ltd. (Advanced Series on Fluid Mechanics)
Subject Category
Research And Support Facilities (Air)
Accession Number
95A88903
Distribution Limits
Public
Copyright
Other

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