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Adaptation of two-dimensional transonic analysis code, TSFOIL, for use in modeling adaptive wall test sectionsThe effects of the elastic deformation of the wind tunnel wall held to a streamline-like shape were simulated numerically. The wall itself is simulated by a finite element model and is allowed to deform under the pressure loading developing in the wind tunnel with an airfoil model present. A modified version of the transonic analysis program, TSFOIL, is then used to determine the resulting flow field with the effects of the deformed wall included, the shape of the wall and the flow field. Once a result from a particular operating condition was obtained, the pressure distribution on the airfoil in the wind tunnel model is compared with solutions generated by TSFOIL in the free air mode.
Document ID
19840010021
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Webb, J.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1984
Publication Information
Publication: A Coop. Program to Stimulate Student Involvement through the MIT Undergraduate Research Opportunity Program
Subject Category
Aerodynamics
Accession Number
84N18089
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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