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Bubble Formation and Detachment in Liquid Flow Under Normal and Reduced GravityTwo-phase flows are present in a wide variety of applications for spacecraft thermal control systems design. Bubble formation and detachment is an integral part of the two-phase flow science. The authors objective is to experimentally investigate the effects of liquid cross velocity, gas velocity, and nozzle diameter on the bubble diameter at detachment under reduced and normal gravity and under relatively low gas flow rates. Results from ground (1 g) and reduced gravity experiments will be presented in this paper. For the 1 g experiment, a flow loop was designed and built to accommodate a range of liquid and gas flow rates. The reduced gravity experiment was conducted on the NASA DC-9 reduced gravity platform using the two-phase flow loop qualified for operation on the low-gravity platform. Flow visualization is accomplished using a high speed 500 frames/s camera. The results suggest that the existence of buoyancy force contributes to the faster detachment of bubbles. Buoyancy helps the detachment process which results in smaller bubbles being formed. In reduced gravity, although drag force is present, the virtual non-existence of buoyant force results in larger bubbles and longer times for detachment. Theoretical predictions are also presented in this paper and seem to agree with the experimental results.
Document ID
19980017195
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Nahra, Henry K.
(NASA Lewis Research Center Cleveland, OH United States)
Kamotani, Y.
(Case Western Reserve Univ. Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1998
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
E-11034
AIAA Paper 98-0732
NAS 1.15:206614
NASA/TM-1998-206614
Report Number: E-11034
Report Number: AIAA Paper 98-0732
Report Number: NAS 1.15:206614
Report Number: NASA/TM-1998-206614
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 12, 1998
End Date: January 15, 1998
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP-962-24-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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