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adverse pressure gradient Aeronautical Engineering assumptions boundary layer profile boundary layer thickness chosen Coefficient of viscosity Committee for Aeronautics comparison completely laminar CORNELL UNIVERSITY LIBRARY cylindrical coordinate data of Fig defined differential equation dimensionless displacement thickness divergent ramp duct entrance duct ramp empirical relationship entire ramp length equation reduces experimental data experimental pressure distribution favorable pressure gradient fully turbulent boundary function fuselage growth initial thickness inlet at low integrals of Eq involving transition kinematic viscosity laminar and turbulent laminar boundary layer low subsonic speeds minimum pressure point momentum equation momentum integral equation momentum thickness Non-dimensional Note obtained planform Pohlhausen form presented for calculating pressure loss pressure recoveries radial ranp Reynolds number School of Aeronautical shape parameter shear stress Static pressure steep adverse pressure Straight divergence Stream velocity submerged air inlet Submerged Inlet THEORETICAL thesis thickness of boundary tho boundary layer tho ramp turbulent boundary layer variation velocity profile