#
Reynolds number
Resource Information
The concept ** Reynolds number** represents the subject, aboutness, idea or notion of resources found in **Houston Public Library**.

The Resource
Reynolds number
Resource Information

The concept

**Reynolds number**represents the subject, aboutness, idea or notion of resources found in**Houston Public Library**.- Label
- Reynolds number

- Source
- nasat

## Context

Context of Reynolds number#### Subject of

- A concept for transition mapping on a 10°-cone in the National Transonic Facility using flow-pressure variation
- A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel
- A generalized wall function
- A kinematically consistent two-point correlation function
- A near-wall Reynolds-stress closure without wall normals : under grant NAG1-1772
- A performance comparison of two small rocket nozzles
- A performance comparison of two small rocket nozzles
- Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers
- Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90
- Aerodynamic characterization of a thin, high-performance airfoil for use in ground fluids testing
- Aerodynamic classification of swept-wing ice accretion
- Aerodynamic effects of high turbulence intensity on a variable-speed power-turbine blade with large incidence and Reynolds number variations
- Aerodynamic effects of simulated ice accretion on a generic transport model
- Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade
- Aerodynamic measurements of a variable-speed power-turbine blade section in a transonic turbine cascade
- Aerodynamics of a transitioning turbine stator over a range of Reynolds numbers
- Aerodynamics of a transitioning turbine stator over a range of Reynolds numbers
- Aerothermal analysis of a wing-elevon cove with variable leakage
- Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions
- An application of a two-equation model of turbulence to three-dimensional chemically reacting flows
- An experimental documentation of trailing-edge flows at high Reynolds number
- Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques
- Application of an upwind high resolution finite-differencing scheme and multigrid method in steady-state incompressible flow simulations
- Application of large-eddy interaction model to channel flow
- Assessment of dual-point drag reduction for an executive-jet modified airfoil section
- Boundary layer transition in the leading edge region of a swept cylinder in high speed flow
- Coherent large-scale structures in high Reynolds number supersonic jets
- Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading
- Computation of sound generated by viscous flow over a circular cylinder
- Computation of sound generated by viscous flow over a circular cylinder
- Computational heat transfer analysis for oscillatory channel flows
- Computations of complex three-dimensional turbulent free jets
- Computer program for calculating flow parameters and power requirements for cryogenic wind tunnels
- Control of unsteady separated flow associated with the dynamic stall of airfoils : final report, 95-09
- Correlation of transonic-cone Preston-tube data and skin friction : final report (research grant number NAG 2-76) (Nov. 80 - May 84)
- Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions
- Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions
- Design guide for aerodynamics testing of Earth and planetary entry vehicles in a ballistic range
- Drag reduction on circular cylinders by ejecting jet from rear stagnation region : progress report for the period ending June 30, 1997 ... under Cooperative Agreement NCC1-232
- Effect of crossflow on Görtler instability in incompressible boundary layers
- Effect of in-flight ice accretion on the performance of a multi-element airfoil
- Effects of droplet interactions on droplet transport at intermediate Reynolds numbers
- Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique
- Experimental investigation of the behavior of sub-grid scale motions in turbulent shear flow : NASA grant NAG 2-382, final report ... funding dates: October 1, 1985 to March 31, 1987
- Experimental measurements of sonic boom signatures using a continuous data acquisition technique
- Experimental optimization methods for multi-element airfoils : final report
- Experimental study of boundary layer flow control using an array of ramp-shaped vortex generators
- Experimental study of saddle point of attachment in laminar juncture flow
- Experimental study of the effects of reynolds number on high angle of attack aerodynamic characteristics of forebodies during rotary motion
- Experimental study of vortex breakdown in a cylindrical, swirling flow
- Experimental surface pressure data obtained on 65 ° delta wing across Reynolds number and Mach number ranges
- Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges
- Experiments on the flow field physics of confluent boundary layers for high-lift systems
- F/A-18 forebody vortex control
- Factors influencing pitot probe centerline displacement in a turbulent supersonic boundary layer
- Factors influencing pitot probe centerline displacement in a turbulent supersonic boundary layer
- Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing
- Flow distribution around the SSME main injector assembly using porosity formulation
- Flow over swept flaps and flap tips : final technical report to NASA Langley Research Center on NAG-1-1614
- Heat transfer in aeropropulsion systems
- Hypersonic lateral and directional stability characteristics of aeroassist flight experiment configuration in air and CF4
- In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0
- Influence of turbulence parameters, Reynolds number, and body shape on stagnation-region heat transfer
- Instability and transition of flow at, and near, an attachment-line : including control by surface suction
- Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results
- Investigation of materials for boundary layer control in a supersonic wind tunnel
- Long hole film cooling dataset for CFD development, Part 1, Infrared thermography and thermocouple surveys
- Low Reynolds number boundary layers in a disturbed environment
- Low-speed wind-tunnel results for symmetrical NASA LS(1)-0013 airfoil
- Mach 6 flow field surveys beneath the forebody of an airbreathing missile
- Mach 6 flow field surveys beneath the forebody of an airbreathing missile
- Magnetic flux compression experiments using plasma armatures
- Mean velocity and turbulence measurements in a 90° curved duct with thin inlet boundary layer : final report
- Mean veoIocity and turbulence measurements in a 900 curved duct with thin inlet boundary layer : final report
- Measurements of heat transfer, flow, and pressures in a simulated turbine blade internal cooling passage
- NASA Dryden Flow Visualization Facility
- NASA Glenn 1-by 1-foot supersonic wind tunnel user manual
- NASA Glenn 1-by 1-foot supersonic wind tunnel user manual
- Navier-Stokes analysis of turbine blade heat transfer
- Navier-Stokes simulation of several high-lift reference H configurations
- Numerical simulation of internal heat transfer phenomena occurring during de-icing of aircraft components : final technical report for NASA grant NAG 3-1796
- On parametric sensitivity of Reynolds-averaged Navier-Stokes SST turbulence model : 2D hypersonic shock-wave boundary-layer interactions
- Overview of HATP experimental aerodynamics data for the baseline F/A-18 configuration : High-Angle-of-Attack Technology Conference
- Perfectly matched layer for linearized Euler equations in open and ducted domains
- Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations
- R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
- Radial and circumferential flow surveys at the inlet and exit of the Space Shuttle Main Engine High Pressure Fuel Turbine model
- Rapport d'essais du profil CAST 10 en transition dʹeclenchʹee, effectuʹes dans la soufflerie transsonique cryogʹenique T2 en pr'esence de parois auto-adaptables : Report on tests of a CAST 10 airfoil with fiexed transition in the T2 transonic cryogenic wind tunnel with self-adaptive walls
- Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate) : under cooperative agreement NCC1-241
- Research and applications in aeroelasticity and structural dynamics at the NASA Langley Research Center
- Research on supersonic inlet bleed
- Results of aerothermodynamic and boundary layer transition testing of 0.0362-Scale X-38 (Rev 3.1) vehicle in NASA Langley 20-inch Mach 6 tunnel
- Reynolds number effects at high angles of attack
- Reynolds number effects on the performance of lateral control devices
- Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine
- Shed vortex structure and phase-averaged velocity statistics in symmetric/asymmetric turbulent flat plate wakes
- Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails
- Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65° delta wings varying in leading-edge radius and camber
- Surface-slip equations for multicomponent, nonequilibrium air flow
- Swept-wing ice accretion characterization and aerodynamics
- Tests of a NACA 651-213 airfoil in the NASA Langley 0.3 meter transonic cryogenic tunnel
- The effects of Reynolds number, rotor incidence angle, and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage
- The effects of anisotropic free-stream turbulence on turbulent boundary layer behavior
- The effects of viscosity on the stability of a trailing-line vortex in compressible flow
- The evolution of condensates in shock tube flow : final technical report, May 1, 1994 to April 30, 1995
- The transition from thick to thin plate wake physics : whither vortex shedding?
- Transonic Navier-Stokes calculations about a 65° delta wing
- Transonic cryogenic test section for the Göttingen tube facility
- Transonic separated flow predictions based on a mathematically simple, nonequilibrium turbulence closure model
- UAS integration in the NAS project : flight test 3 data analysis of JADEM-autoresolver detect and avoid system
- User manual for NASA Lewis 10- by 10-foot supersonic wind tunnel
- Wave phenomena in a high Reynolds number compressible boundary layer
- Wind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds
- Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing
- Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing
- Wind tunnel test of a risk-reduction wing/fuselage model to examine juncture-flow phenomena
- Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3
- Wing pressure distributions from subsonic tests of a high-wing transport model

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