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Gravity Effects in Two-Phase Microgap FlowThe high power density of emerging electronic devices is driving the transition from remote cooling, which relies on conduction and spreading, to embedded cooling, which extracts dissipated heat on-site. Two-phase microgap coolers employ the forced flow of dielectric fluids undergoing phase change in a heated channel within or between devices. Such coolers must work reliably in all orientations for a variety of applications (e.g., vehicle-based equipment), as well as in microgravity and high-g for aerospace applications, but the lack of acceptable models and correlations for orientation- and gravity-independent operation has limited their use. Reliable criteria for achieving orientation- and gravity-independent flow boiling would enable emerging systems to exploit this thermal management technique and streamline the technology development process. As a first step toward understanding the effect of gravity in two-phase microgap flow and transport, in an earlier effort, the authors studied the effects of evaporator orientation, mass flux, and heat flux on flow boiling of HFE7100 in a 1.01 mm tall by 13.0 mm wide by 12.7 mm long microgap channel. Orientation-independence, defined as achieving similar critical heat fluxes, heat transfer coefficients, and flow regimes across orientations, was achieved for mass fluxes of 400 kg/sq.m-s and greater (corresponding to a Froude number of about 0.8). In the present effort, the authors have studied the effects of gravity, mass flux, and subcooling on flow boiling of HFE7100 in a 0.17 mm tall by 13.0 mm wide by 12.7 mm long microgap channel. The Flow Boiling in Microgap Coolers payload experienced about three minutes of weightlessness and shorter periods of high-g (up to about 5 g) during two recent flights aboard the Blue Origin New Shepard reusable launch vehicle. The results from the flight experiments will be presented and compared with published criteria for achieving gravity-independence.



Document ID
20190032578
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Robinson, Franklin L.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Bar-Cohen, Avram
(Maryland Univ. College Park, MD, United States)
Date Acquired
November 7, 2019
Publication Date
October 7, 2019
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
GSFC-E-DAA-TN73788
Report Number: GSFC-E-DAA-TN73788
Meeting Information
Meeting: International Technical Conference and Exhibition on Packaging and Integration of Electronic and Photonic Microsystems (InterPACK)
Location: Anaheim, CA
Country: United States
Start Date: October 7, 2019
End Date: October 9, 2019
Sponsors: American Society of Mechanical Engineers
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
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