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The steady-state flow quality of an open return wind tunnel model.The structural cost of open return wind tunnels is significantly less than that of the more conventional closed return wind tunnels. However, because of the effects of external winds, the flow quality of open return wind tunnels is an area of concern at the low speeds required for V/STOL testing. The development of a configuration which has good flow quality at low as well as at high test speeds is described. The flow quality required at the low test speeds of interest for V/STOL aircraft is discussed and alternatives to the traditional manner of specifying the flow quality requirements in terms of dynamic pressure and angle of attack are suggested.
Document ID
19730030710
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Mort, K. W.
Kelly, M. W.
(NASA Ames Research Center Moffett Field, Calif., United States)
Eckert, W. T.
(NASA Ames Research Center Moffett Field, Calif.; U.S. Army, Air Mobility Research and Development Laboratory, Fort Eustis, Va., United States)
Date Acquired
August 7, 2013
Publication Date
November 1, 1972
Subject Category
Facilities, Research, And Support
Accession Number
73A15512
Distribution Limits
Public
Copyright
Other

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