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The effects of turbulence on droplet drag and secondary droplet breakupThe objective of this research is to obtain an improved understanding of the behavior of droplets in vaporizing sprays, particularly under conditions typical of those in high pressure rocket sprays. Experiments are conducted in a variety of high pressure, high temperature, optically-accessible flow systems, including one which is capable of operation at pressures up to 70 atm, temperatures up to 600 K, gas velocities up to 30 m/sec and turbulence intensities up to 40 percent. Single droplets, 50 to 500 micron in diameter, are produced by an aerodynamic droplet generator and transversely injected into the flow. Measurements are made of the droplet position, size, velocity and temperature and of the droplet's vapor wake from which droplet drag, dispersion, heating, vaporization and breakup are characterized.
Document ID
19950002783
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Song, Y.-H.
(Pennsylvania State Univ. University Park, PA, United States)
Coy, E.
(Pennsylvania State Univ. University Park, PA, United States)
Greenfield, S.
(Pennsylvania State Univ. University Park, PA, United States)
Ondas, M.
(Pennsylvania State Univ. University Park, PA, United States)
Prevish, T.
(Pennsylvania State Univ. University Park, PA, United States)
Spegar, T.
(Pennsylvania State Univ. University Park, PA, United States)
Santavicca, D.
(Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
August 17, 2013
Publication Date
November 1, 1994
Publication Information
Publication: NASA Propulsion Engineering Research Center, Volume 2
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
95N70903
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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