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Limits of adaptation, residual interferencesMethods of determining linear residual wall interference appear to be well established theoretically; however they need to be validated, for example by comparative studies of test data on the same model in different adaptive-wall wind tunnels as well as in passive, ventilated-wall tunnels. The GARTEur CAST 7 and the CAST 10/DOA 2 investigations are excellent examples of such comparative studies. Results to date in both one-variable and two-variable methods for nonlinear wall interference indicate that a great deal more research and validation are required. The status in 2D flow is advanced over that in 3D flow as is the case generally with adaptive-wall development. Nevertheless, it is now well established that for transonic testing with extensive supercritical flow present, significant wall interference is likely to exist in conventional ventilated test sections. Consequently, residual correction procedures require further development hand-in-hand with further adaptive-wall development.
Document ID
19900017528
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mokry, Miroslav
(National Aerospace Lab. Amsterdam (Netherlands)., United States)
Erickson, J. C., Jr.
(National Aerospace Lab. Amsterdam (Netherlands)., United States)
Goodyer, Michael J.
(National Aerospace Lab. Amsterdam (Netherlands)., United States)
Mignosi, Andre
(National Aerospace Lab. Amsterdam (Netherlands)., United States)
Russo, Giuseppe P.
(National Aerospace Lab. Amsterdam (Netherlands)., United States)
Smith, J.
(National Aerospace Lab. Amsterdam (Netherlands)., United States)
Wedemeyer, Erich H.
(Deutsche Forschungs- und Versuchsanstalt fuer Luft- und Raumfahrt, Goettingen, Germany F.R. , United States)
Newman, Perry A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
April 1, 1990
Publication Information
Publication: AGARD, Fluid Dynamics Panel Working Group 12 on Adaptive Wind Tunnel Walls: Technology and Applications
Subject Category
Research And Support Facilities (Air)
Accession Number
90N26844
Distribution Limits
Public
Copyright
Other
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