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Mechanism of Supercooled Water Droplet Breakup near the Leading Edge of an AirfoilThis work presents the results of an experimental study on supercooled droplet deformation and breakup near the leading edge of an airfoil. The results are compared to prior room temperature droplet deformation results to explore the effects of droplet supercooling. The experiments were conducted in the Adverse Environment Rotor Test Stand (AERTS) at The Pennsylvania State University. An airfoil model placed at the end of the rotor blades mounted onto the hub in the AERTS chamber was moved at speeds ranging between 50 and 80 m/sec. The temperature of the chamber was set at -20˚C. A monotonic droplet generator was used to produce droplets that fell from above, perpendicular to the path of the airfoil. The supercooled state of the droplets was determined by measurement of the temperature of the drops at various locations below the droplet generator exit. A temperature prediction code was also used to estimate the temperature of the droplets based on vertical velocity and the distance traveled by droplets from the droplet generator to the airfoil stagnation line. High speed imaging was employed to observe the interaction between the droplets and the airfoil. The high speed imaging provided droplet deformation information as the droplet approached the airfoil near the stagnation line. A tracking software program was used to measure the horizontal and vertical displacement of the droplet against time. It was demonstrated that to compare the effects of water supercooling on droplet deformation, the ratio of the slip velocity and the initial droplet velocity must be equal. A case with equal slip velocity to initial velocity ratios was selected for room temperature and supercooled droplet conditions. The airfoil velocity was 60 m/s and the slip velocity for both sets of data was 40 m/s. In these cases, the deformation of the weakly supercooled and warm droplets did not present different trends. The similar behavior for both environmental conditions indicates that water supercooling has no effect on particle deformation for the limited range of the weak supercooling of the droplets tested and the selected impact velocity. The assumption of a constant surface tension value was further supported by the equal trend of the Bond number obtained for supercooled and room temperature droplets.
Document ID
20170007704
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Veras-Alba, Belen
(Pennsylvania State Univ. State College, PA, United States)
Palacios, Jose
(Pennsylvania State Univ. State College, PA, United States)
Vargas, Mario
(NASA Glenn Research Center Cleveland, OH United States)
Ruggeri, Charles
(NASA Glenn Research Center Cleveland, OH United States)
Bartkus, Tadas P.
(Ohio Aerospace Inst. Cleveland, OH, United States)
Date Acquired
August 11, 2017
Publication Date
June 5, 2017
Subject Category
Air Transportation And Safety
Fluid Mechanics And Thermodynamics
Numerical Analysis
Report/Patent Number
GRC-E-DAA-TN42773
Meeting Information
Meeting: AIAA Atmospheric and Space Environments Conference 2017
Location: Denver, CO
Country: United States
Start Date: June 5, 2017
End Date: June 9, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 081876.02.03.08.02.02
CONTRACT_GRANT: NNC13BA10B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
in-flight icing
droplet breakup
icing physics
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