ASME Winter Anual
(20/Nov/97 in Dallas)

アメリカ機械学会
発表予定論文

Index

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  項目
ABSTRACT
INTRODUCTION
EXPERIMENTAL
RESULTS AND DISCUSSION
CONCLUDING REMARKS

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PARABOLIC FLIGHT EXPERIMENTS OF SPRAY COOLING WITH WATER AND FC-72
UNDER REDUCED AND ELEVATED GRAVITY

Ken-ichi YOSHIDA, Takahisa KATO
Department of Mechanical Engineering
Keio University, Yokohama, Japan

Toshiharu OKA
Research Institute, Ishikawajima-Harima Heavy
Industries Co., Ltd, Yokohama, Japan

Yoshiyuki ABE
Electrotechnical Laboratory,
Tsukuba, Ibaraki, Japan

Yasuhiko H. MORI, Akira NAGASHIMA
Department of Mechanical Engineering
Keio University, Yokohama, Japan

ABSTRACT
  This paper reports on the authors* latest parabolic-flight experiments (November 1996) of spray cooling. Water and FC-72 (perfluorocarbon) were employed alternately as a test liquid sprayed from a single full-cone nozzle onto a Cr-plated surface of an electrically heated copper block (transient cooling experiments) or onto a transparent In2O3-coated surface of a glass block (steady state experiments in a relatively low superheat region). Each experimental run was accomplished during some 15 seconds through which a reduced gravity condition (〜0.01 times the terrestrial gravity) or an elevated gravity condition (〜2 times the terrestrial gravity) was maintained in the laboratory used - the cabin of an MU-300 aircraft. Cooling curves over a wide range of wall-superheat were obtained with water sprayed at significantly different volume fluxes and with FC-72 sprayed at rather low volume fluxes. It is demonstrated that the gravity dependency of the spray cooling characteristics varies with the spray volume flux and the impinging droplet velocity. Qualitative interpretations of the observed gravity dependency are provided.

NOMENCLATURE
dm : droplet diameter (mm)
Dm: spray volume flux (m3/(m2・s))
ge: terrestrial value of gravity acceleration (m/s2)
q : heat flux (kW/m2)
qCHF: critical heat flux (kW/m2)
Vm : droplet velocity (m/s)
DTsat: superheating of heater surface above saturation temperature (K)



INTRODUCTION
  Spray cooling has been widely applied to many industrial processes in which rapid and effective cooling is required. Because of its capability for intensive and accurately controlled heat removal, spray cooling is considered to be one of the key technologies for developing thermal management systems for use in space. Despite the mass of literature on spray cooling, the present understanding of the effect of gravity on spray cooling characteristics is far from complete. In fact, the present authors* preceding studies(1-3) using parabolic flights of a 15-m jet plane, Mitsubishi MU-300, are the only published efforts directed to clarifying the gravity effect on spray cooling. This paper aims to report on the authors* new series of experiments which was planned to supplement the preceding studies(1-3). Before describing those latest experiments in subsequent sections, the authors* preceding studies are briefly reviewed below.
  The authors* first attempt at evaluating the gravity effect on spray cooling characteristics was performed with water and CFC-113 each sprayed onto a Ni-plated surface of a copper block heater of 19 mm in diameter(1,2). The second attempt employed water and FC-72 (perfluorocarbon), instead of CFC-113, each of which was sprayed onto a Cr-plated surface of a copper block heater of 50-mm in diameter and also onto a metallized surface of a transparent glass heater for observing the behavior of liquid droplets impinging and having impinged on it(3). The major findings obtained in these studies may be summarized as follows. For water:
1. At spray volume fluxes below 3.0×10-4 m3/(m2.s), the heat transfer in the film boiling region beyond the MHF (minimum heat flux) point is degraded by about 30% with a decrease in gravity.


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