A Theoretical Investigation of the Boundary Layer Growth Along the Ramp of a Submerged Air Inlet |
Common terms and phrases
adverse pressure gradient Aeronautical Engineering CORNELL begin the integration BOUNDARY LAYER GROWTH boundary layer profile boundary layer thickness comparison completely laminar CONFIDENT CONFIDENTIAL coordinate CORNELL UNIVERSITY LIBRARY cylindrical coördinate system differential equation displacement thickness duct entrance duct ramp empirical relationship Engineering CORNELL UNIVERSITY entire ramp length experimental data experimental pressure distribution fully turbulent boundary function fuselage given pressure distribution Ho-Po inlet at low integrals of Eq involving transition k₂ Kármán momentum kinematic viscosity laminar and turbulent laminar boundary layer low subsonic speeds minimum pressure point momentum integral equation momentum thickness Non-dimensional Note number and pressure obtained planform Pohlhausen form Prandtl pressure losses pressure recoveries pudy put into dimensionless RAMP SURFACE RAMP WALL Reynolds number shape parameter shear stress variable steep adverse pressure STRAIGHT DIVERGENT RAMP SUBMERGED AIR INLET SUBMERGED INLET Thesis thickness of boundary turbulent boundary layer u)dy variation velocity profile ΔΗ бу ду Мо