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A study of the accuracy of neutrally buoyant bubbles used as flow tracers in airResearch has been performed to determine the accuracy of neutrally buoyant and near neutrally buoyant bubbles used as flow tracers in air. Theoretical, computational, and experimental results are presented to evaluate the dynamics of bubble trajectories and factors affecting their ability to trace flow-field streamlines. The equation of motion for a single bubble was obtained and evaluated using a computational scheme to determine the factors which affect a bubble's trajectory. A two-dimensional experiment was also conducted to experimentally determine bubble trajectories in the stagnation region of NACA 0012 airfoil at 0 deg angle of attack using a commercially available helium bubble generation system. Physical properties of the experimental bubble trajectories were estimated using the computational scheme. These properties included the density ratio and diameter of the individual bubbles. the helium bubble system was then used to visualize and document the flow field about a 30 deg swept semispan wing with simulated glaze ice. Results were compared to Navier-Stokes calculations and surface oil flow visualization. The theoretical and computational analysis have shown that neutrally buoyant bubbles will trace even the most complex flow patterns. Experimental analysis revealed that the use of bubbles to trace flow patterns should be limited to qualitative measurements unless care is taken to ensure neutral buoyancy. This is due to the difficulty in the production of neutrally buoyant bubbles.
Document ID
19930014210
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kerho, Michael F.
(Illinois Univ. Urbana, IL, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1993
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:191088
NASA-CR-191088
E-7630
Report Number: NAS 1.26:191088
Report Number: NASA-CR-191088
Report Number: E-7630
Accession Number
93N23399
Funding Number(s)
CONTRACT_GRANT: NAG3-1134
PROJECT: RTOP 505-68-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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