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EFFECT OF COMPRESSIBILITY OF AIR FLOW AROUND CYLINDER
APPARATUS AND PROCEDURE FOR MEASURING LIQUIDWATER
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accrued error amount of ice angle of impingement appendix approximately assumed droplet-size distribution average calculated curves cloud composed collected per unit content and droplet critical line critical value curves of figure cylinder diameter cylinder method cylinder radius cylinder set cylinder surface data points determined differential analyzer dimensionless diom droplet diameter droplet impingement droplet sizes effect of compressibility entered as item enthalpy equation factor figure 12 flight data free-stream velocity function hodograph ice collected impingement rate incompressible flow field indicated airspeed inertia parameter liquid-water content logarithmic graph paper mass of ice microns miles per hour obtained over-all weighted collection plotted pressure altitude radians rate of ice ratio Reynolds number ROTATING MULTICYLINDER METHOD run-off line shown in figure standard value subcritical supercooled tangent trajectory tion true airspeed unit frontal area value of K0<p volume freezing rate volume-median droplet w*Eu water impingement weighted collection efficiency wfEu