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

The Resource
Air flow
Resource Information

The concept

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

- Authority link
- http://id.worldcat.org/fast/00802370

- Source
- fast

## Context

Context of Air flow#### Subject of

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- A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory
- A new method of testing models in wind tunnels
- A study of hypersonic small-disturbance theory
- A survey of methods for turbojet thrust measurement applicable to flight installation
- A theoretical and experimental study of wind-tunnel-wall effects on oscillating air forces for two-dimensional subsonic compressible flow
- A variable-geometry annular cascade-type inlet at Mach numbers of 1.9 and 3.05
- A visualization study of secondary flows in cascades
- Air flow management in raised floor data centers
- Air flow tests of a narrow collector passage with eight transverse feeder slots : (applicable to 140E1 forward shield design studies)
- Air-flow and performance characteristics of engine-stage supercharger of a double-row radial aircraft engine : 2 - Effect of design variables
- Air-flow and power characteristics of the Langley 16-foot transonic tunnel with slotted test section
- Air-flow surveys in the vicinity of representative NACA 1-series cowlings
- An experimental investigation of transonic flow past two-dimensional wedge and circular-arc sections using a Mach-Zehnder interferometer
- An inlet design concept to reduce flow distortion at angle of attack
- An investigation of the backflow phenomenon in centrifugal superchargers
- Analysis of turbulent heat transfer and flow in the entrance regions of smooth passages
- Approximate solutions for the flow about flat-top wing-body configurations at high supersonic airspeeds
- Approximate turbulent boundary-layer development in plane compressible flow along thermally insulated surfaces with application to supersonic-tunnel contour correction
- Attainable circulation of airfoils in cascade
- Calculation of compressible potential flow past slender bodies of revolution by an integral method
- Charge-air distribution among the cylinders of a double-row radial aircraft engine
- Collection and analysis of hinge-moment data on control-surface tabs
- Comparative effectiveness of a convection-type and a radiation-type cooling cap on a turbosupercharger
- Comparison of experimentally and analytically determined windmilling characteristics of a compressor with low over-all pressure ratio
- Comparison of secondary flows and boundary-layer accumulations in several turbine nozzles
- Component performance investigation of J71 experimental turbine, [Part] V, Effect of third stage shrouding on internal-flow conditions of J71-97 turbine
- Concerning the flow about ring-shaped cowlings : Part 8 - Further measurements on annular profiles
- Considerations on the effect of wind-tunnel walls on oscillating air forces for two-dimensional subsonic compressible flow
- Correspondence flows for wings in linearized potential fields at subsonic and supersonic speeds
- Criteria for initial flow reversal in symmetrical twin-intake air-induction systems operating at supersonic speeds
- Design of injectors for low-pressure air flow
- Design of two-dimensional channels with prescribed velocity distributions along the channel walls, [Part] 2, Solution by Green's function
- Diffusion of heat from a line source in isotropic turbulence
- Downwash, sidewash, and wave survey behind a 42° sweptback wing at a Reynolds number of 6.8 x 106 with and without a simulated ground
- Effect of Mach number on the flow and application of compressibility corrections in a two-dimensional subsonic-transonic compressor cascade having varied porous-wall suction at the blade tips
- Effect of variable viscosity and thermal conductivity on high-speed slip flow between concentric cylinders
- Effects of aspect ratio on air flow at a high subsonic mach numbers
- Effects of wing-body geometry on the lateral-flow angularities at subsonic speeds
- Experimental aerodynamic derivatives of a sinusoidally oscillating airfoil in two-dimensional flow
- Experimental investigation of loss in an annular cascade of turbine-nozzle blades of free vortex design
- Extension of the theory of oscillating airfoils of finite span in subsonic compressible flow
- Flow modulation and fluid-structure interaction at airplane wings : research results of the collaborative research center SFB 401 at RWTH Aachen, University of Technology, Aachen, Germany
- Flow over a slender body of revolution at supersonic velocities
- Flow through cascades in tandem
- Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99, [Part] 2, Isentropic-spike all-external compression inlet
- Generalization of boundary-layer momentum-integral equations to three-dimensional flows including those of rotating system
- Heat transfer from high-temperature surfaces to fluids, [Part] 1, Preliminary investigation with air in inconel tube with rounded entrance, inside diameter of 0.4 inch and length of 24 inches
- Heat transfer from high-temperature surfaces to fluids, [Part] 2, Correlation of heat-transfer and friction data for air flowing in inconel tube with rounded entrance
- Heat transfer on an afterbody immersed in the separated wake of a hemisphere
- Heat, mass, and momentum transfer for flow over a flat plate with blowing or suction
- Horizontal buoyancy in wind tunnels
- 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 span and load per square meter on the air forces of the supporting surface
- Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles
- Investigation of an asymmetric "penshape" exit having circular projections and discharging into quiescent air
- Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds
- Investigation of the penetration of an air jet directed perpendicularly to an air stream
- Investigation of three types of supersonic diffuser over a range of Mach numbers from 1.75 to 2.74
- Investigation of turbulent flow in a two-dimensional channel
- MGCR heat-exchanger test program interim report : isothermal air and helium tests
- Mach tables for real gas equilibrium flow of air in hypervelocity test facilities with total temperatures to 10,000°K
- Note on the accuracy of a method for rapidly calculating the increments in velocity about an airfoil due to angle of attack
- Note on the air forces on a wing caused by pitching
- Note on the resistance of polished cylinders (and cylindrical wires) with generatrices perpendicular to the airstream
- Notes on aerodynamic forces, I, Rectilinear motion
- Notes on aerodynamic forces, II, Curvilinear motion
- Notes on propeller design, II, The distribution of thrust over a propeller blade
- Notes on propeller design, III, The aerodynamical equations of the propeller blade elements
- Notes on propeller design, IV, General proceeding in design
- On a source-sink method for the solution of the Prandtl-Busemann iteration equations in two-dimensional compressible flow
- On the Second-order tunnel-wall-constriction corrections in two-dimensional compressible flow
- On the theory of oscillating airfoils of finite span in subsonic compressible flow
- One-dimensional analysis of choked-flow turbines
- Preliminary attempts at isothermal compression of a supersonic air stream
- Preliminary investigation at low speeds of swept wings in rolling flow
- Pressure measurements on a body of revolution in the Langley 16-foot transonic tunnel and a comparison with free-fall data
- Reduction in efficiency of propellers due to slipstream
- Similarity laws for transonic flow about wings of finite span
- Simultaneous single element air temperature and velocity measurements
- Spectrum of turbulence in a contracting stream
- Studies of flow distribution in the core of a quarter-scale flow model of the PWR reactor
- Study of secondary-flow patterns in an annular cascade of turbine nozzle blades with vortex design
- Supplementary model studies of flow distribution in the core of the PWR reactor
- Tables and charts for the evaluation of profile drag from wake surveys at high subsonic speeds
- Tests of a small-scale NACA submerged inlet at transonic Mach numbers
- The determination of downwash
- The effect of increase in combustion-air inlet temperature from 80 to 130 degrees F on the sea-level performance of a 22-inch-diameter pulse-jet engine
- The effect on rudder control of slip stream body, and ground interference
- The normal component of the induced velocity in the vicinity of a lifting rotor and some examples of its application
- The reversibility theorem for thin airfoils in subsonic and supersonic flow
- Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross-sectional areas
- Theoretical and experimental investigation of the effect of tunnel walls on the forces on an oscillating airfoil in two-dimensional subsonic compressible flow
- Theoretical and experimental investigation of the subsonic-flow fields beneath swept and unswept wings with tails of vortex-induced velocities
- Theoretical investigation of transonic similarity for bodies of revolution
- Theoretical relations between the stability derivatives of a wing in direct and in reverse supersonic flow
- Theoretical span load distributions and rolling moments for sideslipping wings of arbitrary plan form in incompressible flow
- Transonic flow past a wedge profile with detached bow wave : general analytical method and final calculated results
- Two-dimensional compressible flow in centrifugal compressors with logarithmic-spiral blades
- Two-dimensional transonic flow past airfoils
- Velocity distributions on symmetrical airfoils in closed tunnels by conformal mapping

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