#
Boundary layer
Resource Information
The concept ** Boundary layer** represents the subject, aboutness, idea or notion of resources found in **University of Oklahoma Libraries**.

The Resource
Boundary layer
Resource Information

The concept

**Boundary layer**represents the subject, aboutness, idea or notion of resources found in**University of Oklahoma Libraries**.- Label
- Boundary layer

- Authority link
- http://id.worldcat.org/fast/00837095

- Source
- fast

## Context

Context of Boundary layer#### Subject of

- A method for the design of porous-wall wind tunnels
- A study of velocity profiles in the momentum integral method with slip boundary conditions
- A visualization study of secondary flows in cascades
- An Experimental investigation of the effect of surface heating on boundary-layer transition on a flat plate in supersonic flow
- An investigation of a thermal ice-prevention system for a C-46 cargo airplane : 1 - Analysis of the thermal design for wings, empennage, and windshield
- Analysis of turbulent free-convection boundary layer on flat plate
- Atmospheric transmittance from 0.25 to 28.5 micrometers : supplement LOWTRAN 3B (1976)
- Attainable circulation of airfoils in cascade
- Average skin-friction coefficients from boundary-layer measurements on an ogive-cylinder body in flight at supersonic speeds
- Basic experimental study of the coupling between flow instabilities and incident sound
- Blending of Surface and Rawinsonde Data in Mesoscale Objective Analysis
- Boundary and interior layers, computational and asymptotic methods -- BAIL 2014
- Boundary layer studies on a spinning cone
- Boundary-layer measurements on several porous materials with suction applied
- Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue
- Calculation of the velocity profiles of the incompressible laminar boundary layer on a yawed spinning cone and the magnus effect
- Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment
- Characteristics of the sidewall and floor boundary layers in BRL supersonic wind tunnel no. 1
- Comparison of results of experimental and theoretical studies of blade-outlet boundary-layer characteristics of stator blade for a high subsonic Mach number turbine
- Comparison of secondary flows and boundary-layer accumulations in several turbine nozzles
- Compressible turbulent boundary layer computations for flow with longitudinal curvature
- Contributions of a wall shear stress to the Magnus effect on nose shapes
- Correlation parameters for two-dimensional jet interaction
- Exact solutions of laminar-boundary-layer equations with constant property values for porous wall with variable temperature
- Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities
- Experimental investigation of temperature recovery factors on bodies of revolution at supersonic speeds
- Experimental investigation of the mixing loss behind trailing edge of a cascade of three 90° supersonic turning passages
- Factors affecting transition at supersonic speeds
- Flight-measured laminar boundary layer transition phenomena including stability theory analysis
- Heat transfer to blunt nose shapes with laminar boundary layers at high supersonic speeds
- Heat, mass, and momentum transfer for flow over a flat plate with blowing or suction
- Hermite interpolation algorithm for constructing reasonable analytic curves through discrete data points
- Hyperbolic/parabolic development for the GIM-STAR code
- IUTAM Symposium on One Hundred Years of Boundary Layer Research : proceedings of the IUTAM symposium held at DLR-Göttingen, Germany, August 12-14, 2004
- Influence of wall boundary layer upon the performance of an axial-flow fan rotor
- Influence of wall boundary layer upon the performance of an axial-flow fan rotor
- Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles
- Investigation at transonic speeds of aerodynamic characteristics of an unswept semielliptical air inlet in the root of a 45° sweptback wing
- Investigation of a simple device for preventing separation due to shock and boundary-layer interaction
- Low-speed wind-tunnel investigation of a triangular sweptback air inlet in the root of a 45 degree sweptback wing
- Mach 6 flow field surveys beneath the forebody of an airbreathing missile
- Normal force, center of pressure, and zero-lift drag of several ballistic-type missiles at Mach numbers of 4.05
- On the use of a scale-dependent filter in channel model integrations
- Preliminary investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61
- Preliminary results from a free-flight investigation of boundary-layer transition and heat transfer on a highly polished 8-inch-diameter hemisphere-cylinder at Mach numbers up to 3 and Reynolds numbers based on a length of 1 foot up to 17.7 x 106
- Preliminary surveys of the three dimensional boundary layer on a yawed, spinning body of revolution
- R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
- Recent results in laminar-turbulent transition : selected numerical and experimental contributions from the DFG Priority Programme 'Transition' in Germany
- Small viscosity and boundary layer methods : theory, stability analysis, and applications
- The boundary layer in the confinement of a one-dimensional plasma
- The effect of the inlet mach number and inlet-boundary-layer thickness on the performance of a 23° conical-diffuser-tail-pipe combination
- The use of a luminescent lacquer for the visual indication of boundary-layer transition
- Three-dimensional attached viscous flow : basic principles and theoretical foundations
- Transportation of bed material due to wave action
- Vertical profiles of wind speeds from measurements of high towers
- Wall heat transfer effects on supersonic nozzle wall boundary-layer temperature profiles
- Wind-tunnel investigation of the boundary layer on an NACA 0009 airfoil having 0.25- and 0.50-airfoil chord plain sealed flaps
- Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3

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`<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.libraries.ou.edu/resource/E6Unlh0xLLU/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.libraries.ou.edu/resource/E6Unlh0xLLU/">Boundary layer</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.libraries.ou.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.libraries.ou.edu/">University of Oklahoma Libraries</a></span></span></span></span></div>`