Effects of Rotation on Coolant Passage Heat Transfer, Volume 1; Volume 4396
National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991 - Heat
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AP/P)in axis of rotation baseline flow condition BCD EF GHI boundary layer buoyancy forces buoyancy parameter channel Coolant Passage Heat Coriolis forces correlation DATA BAND decreases Displacement Thickness Eckert effects of rotation FLAGS ROTATION NUMBER flow direction gas turbine GHI JK GUARD heat transfer coefficients heat transfer experiments heat transfer model heat transfer ratio heat transfer results high pressure side high pressure surfaces hydraulic diameter increase in heat JK GUARD OUTWARD laminar leading and trailing leading surface low pressure surface Low Rotation nondimensional nonrotating Nusselt number outward flowing passage Passage Heat Transfer radially outward flow ratio distribution Reynolds number Rotating Heat Transfer second passage SECOND STRAIGHT TURN secondary flow shown in Figure side walls skin friction straight passage STRAIGHT TURN STRAIGHT STRAIGHT TURN STREAMWISE SYMBOL FLAGS ROTATION test conditions TEST SECTION SURFACES test surface thermocouples trailing side trailing surfaces turbulent TURN STRAIGHT TURN TURN STREAMWISE LOCATION Variation of Heat