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Experimental investigations on the V/STOL tunnel at NASA/Langley Research CenterThe flow characteristics of the V/STOL tunnel were investigated. The results show an interaction between tunnel components. The flow around the tunnel circuit gradually deteriorated with increasing distance from the testing area. The flow in the first diffuser was still satisfactory at the beginning of the circuit, while at the end of the circuit, the flow approaching the contraction became entirely unsatisfactory. Deterioration of flow was due largely to turning the stream around the corners, with the resulting flow distortion affecting the diffusers downstream. The large end of the last diffuser stalled on one side and nearly stalled the flow at the tip of the fan. It was found that these adverse flow characteristics reduce the flow quality and the efficiency of the tunnel.
Document ID
19810011500
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Barna, P. S.
(Barna (P. Stephen), Consultant Norfolk, VA, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1981
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-165655
Report Number: NASA-CR-165655
Accession Number
81N20028
Funding Number(s)
CONTRACT_GRANT: NASA ORDER L-12343-B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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