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The steady-state flow quality in a model of a non-return wind tunnelThe structural cost of non-return wind tunnels is significantly less than that of the more conventional closed-circuit wind tunnels. However, because of the effects of external winds, the flow quality of non-return wind tunnels is an area of concern at the low test speeds required for V/STOL testing. The flow quality required at these low speeds is discussed and alternatives to the traditional manner of specifying the flow quality requirements in terms of dynamic pressure and angularity are suggested. The development of a non-return wind tunnel configuration which has good flow quality at low as well as at high test speeds is described.
Document ID
19720023636
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mort, K. W.
(NASA Ames Research Center Moffett Field, CA, United States)
Eckert, W. T.
(NASA Ames Research Center Moffett Field, CA, United States)
Kelly, M. W.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1972
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-TM-X-62170
Report Number: NASA-TM-X-62170
Accession Number
72N31286
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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