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Development of minimum correction wind tunnelsFlow distortions due to wind tunnel wall interference may be accounted for if the model to tunnel ratio is small, but the theory becomes less reliable as the model becomes larger. This paper presents theoretical analysis and experimental evidence which supports a new concept of wind tunnel. The method employs active control of flow through the walls so that the model is in approximately free air conditions during the test. Practical considerations in the design of such a tunnel are presented. Results indicate that a minimum correction wind tunnel may be achieved with active walls of relatively low porosity.
Document ID
19750034270
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bernstein, S.
Joppa, R. G.
(Washington, University Seattle, Wash., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 75-144
Report Number: AIAA PAPER 75-144
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: Pasadena, CA
Start Date: January 20, 1975
End Date: January 22, 1975
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
75A18342
Funding Number(s)
CONTRACT_GRANT: NGL-48-002-010
Distribution Limits
Public
Copyright
Other

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