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Unsteady density and velocity measurements in the 6 foot x 6 foot wind tunnelThe methods used and the results obtained in four aero-optic tests are summarized. It is concluded that the rather large values of density fluctuation appear to be the result of much higher Mach number than freestream and the violent turbulence in the flow as it separates from the turret. A representative comparison of fairing on-fairing off rms density fluctuation indicates essentially no effect at M = 0.62 and a small effect at M = 0.95. These data indicate that some slight improvement in optical quality can be expected with the addition of a fairing, although at M = 0.62 its effect would be nil. Fairings are very useful in controlling pressure loads on turrets, but will not have first order effects on optical quality. Scale sizes increase dramatically with increasing azimuth angle for a reprensentative condition. Since both scale sizes and fluctuation levels increase (total turbulence path length also increases) with azimuth angle, substantial optical degradation might be expected. For shorter wave lengths, large degradations occur.
Document ID
19800017097
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rose, W. C.
(Rose Eng. and Res., Inc. Moffett Field, CA, United States)
Johnson, D. A.
(NASA Ames Research Center)
Date Acquired
August 10, 2013
Publication Date
April 1, 1980
Publication Information
Publication: Proc. of the Aero-Optics Symp. on Electromagnetic Wave Propagation from Aircraft
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
80N25594
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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