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air flow airfoil airplane altitude angle of attack baffle balancing plate blower brake horsepower calculated characteristics circular tubes COMMITTEE FOR AERONAUTICS compression constant control surface cooling air cooling-air pressure drop counterflow cowling crossflow curve cylinder density diameter diffuser distribution drag duct dynamic pressure effect engine-air entrance exit form drag free-stream frontal area fuel fuel—air ratio function fuselage heat exchanger heat transfer heat-transfer coefficient hinge-moment horsepower hot fluid hydraulic diameter inch increase inlet temperature installation intercooler internal balance laminar flow Langley Field lift coefficient loss in total mean temperature difference NACA NACA cowling NATIONAL ADVISORY COMMITTEE Nusselt oil coolers orifice plate percent power cost radiator rate of heat reference Reynolds number selection chart shear and direct shown in figure square foot static pressure station supercharger surface area tests tion total pressure turbulent flow variables variation velocity vent location wing