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On optical imaging through aircraft turbulent boundary layersOptical resolution quality as affected by aircraft turbulent boundary layers is analyzed. Wind-tunnel data was analyzed to obtained the variation of boundary layer turbulence scale length and mass density rms fluctuations with Mach number. The data gave good agreement with a mass density fluctuation turbulence spectrum that is either isotropic of orthogonally anisotropic. The data did not match an isotropic turbulence velocity spectrum which causes an anisotropic non-orthogonal mass density fluctuation spectrum. The results indicate that the average mass density rms fluctuation is about 10% of the maximum mass density across the boundary layer and that the transverse turbulence scale size is about 10% of the boundary layer thickness. The results indicate that the effect of the turbulent boundary layer is large angle scattering which decreases contrast but not resolution. Using extinction as a criteria the range of acceptable aircraft operating conditions are given.
Document ID
19800017099
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sutton, G. W.
(Avco-Everett Research Lab. MA, United States)
Date Acquired
August 10, 2013
Publication Date
April 1, 1980
Publication Information
Publication: NASA. Ames Res. Center Proc. of the Aero-Optics Symp. on Electromagnetic Wave Propagation from Aircraft
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AMP-334
Report Number: AMP-334
Accession Number
80N25596
Funding Number(s)
CONTRACT_GRANT: F19628-70-C-0230
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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