PREDICTION AND RATIONAL CORRELATION OF THERMOPHORETICALLY REDUCED PARTICLE MASS TRANSFER TO HOT SURFACES ACROSS LAMINAR OR TURBULENT FORCED-CONVECTION GAS BOUNDARY LAYERS†

REFERENCES

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• This research was supported in part by NASA Lewis Research Center (Grants NAG 3-590 and NCC 3-45)and U.S. Air Force Office of Scientific Research (Grant AFOSR-84–0034)
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