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

The Resource
Reynolds number
Resource Information

The concept

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

- Authority link
- (EG-IN)625656

## Context

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- Water-tunnel study of transition flow around circular cylinders
- A finite Reynolds number approach for the prediction of boundary layer receptivity in localized regions
- A finite element computational method for high Reynolds number laminar flows
- A hybridized method for computing high-reynolds-number hypersonic flow about blunt bodies
- A realizable Reynolds stress algebraic equation model
- A review of some Reynolds number effects related to bodies at high angles of attack
- A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel
- 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 performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-meter Transonic Cryogenic Tunnel
- An approximate method for estimating the critical Reynolds number for a heated flat plate in water
- An efficient and robust algorithm for two dimensional time dependent incompressible Navier-Stokes equations : high Reynolds number flows
- An experimental and analytical investigation of the effect on isolated boattail drag of varying Reynolds number up to 130 x 106
- An experimental documentation of trailing-edge flows at high Reynolds number
- An investigation of turbulence structure in a low-Reynolds-number incompressible turbulent boundary : final report
- Analysis of fluctuating static pressure measurements in a large high Reynolds number transonic cryogenic wind tunnel
- Coherent large-scale structures in high Reynolds number supersonic jets
- Comment on "Local energy transfer and nonlocal interactions in homogeneous, isotropic turbulence" [Phys. Fluids A2, 413 (1990)]
- Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds
- Cryogenic wind technology : a way to measurement at higher Reynolds numbers
- Cryogenic wind tunnels for high Reynolds number testing
- Drag 'n' fly : a proposal in response to a low Reynolds number station keeping mission
- Effect of Reynolds number and Mach number on flow angularity probe sensitivity
- Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations
- Effect of Reynolds number variation on aerodynamics of a hydrogen-fueled transport concept at Mach 6
- Effects of global density and Reynolds number variations on mixing in turbulent, axisymmetric jets
- Effects of independent variation of Mach and Reynolds numbers on the low-speed aerodynamic characteristics of the NACA 0012 airfoil section
- Effects of large-scale intermittency of turbulence on scalar spectra at high wave numbers
- Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
- Elliptic flow computation by low Reynolds number two-equation turbulence models
- Evaluation of high reynolds number flow in a 180 degree turn-around duct
- Experimental investigation to validate use of cryogenic temperatures to achieve high Reynolds numbers in boattail pressure testing
- Fast methods to numerically integrate the Reynolds equation for gas fluid films
- Final design proposal : Dawdler : a proposal in response to a low Reynolds number station keeping mission
- Final design proposal : the MANTA : an RPV designed to investigate forces and moments on a lifting surface
- Final report for the grant integration of viscous effects into inviscid computational methods
- Flight Mechanics/Estimation Theory Symposium, 1989 : proceedings of a symposium sponsored by NASA Goddard Space Flight Center and held at Goddard Space Flight Center, Greenbelt, Maryland, May 23-24, 1989
- Further development of a method for computing three-dimensional subsonic viscous flows in turbofan lobe mixers
- High Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-meter transonic cryogenic tunnel
- High Reynolds number tests of a NASA SC(3)-0712(b) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnels
- High Reynolds number tests of the NASA SC(2)-0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
- High Reynolds number tests of the cast 10-2/DOA 2 airfoil in the Langley 0.3-meter transonic cryogenic tunnel - phase II
- High-resolution liquid crystal heat transfer measurements on the end wall of a turbine passage with variations in Reynolds number
- Highlights of unsteady pressure tests on a 14 percent supercritical airfoil at high Reynolds number, transonic condition
- Hot-jet simulation in cryogenic wind tunnels
- Investigation of the validity of Reynolds averaged turbulence models at the frequencies that occur in turbomachinery
- Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip
- Low-speed tests of a high-aspect-ratio, supercritical-wing transport model equipped with a high-lift flap system in the Langley 4- by 7-meter and Ames 12-foot pressure tunnels
- Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel
- Numerical solution for the velocity-derivative skewness of a low-Reynolds-number decaying Navier-Stokes flow
- On the drag of model dendrite fragments at low Reynolds number
- On the modeling of low-Reynolds-number turbulence
- Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
- R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
- Representation of turbulent shear stress by a product of mean velocity differences
- Reynolds number influences in aeronautics
- Reynolds number tests of an NPL 9510 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
- Reynolds-stress and dissipation rate budgets in a turbulent channel flow
- Solution of the Euler equations with viscous-inviscid interaction for high Reynolds number transonic flow past wing/body configurations
- Static aerodynamic characteristics of a typical single-engine low-wing general aviation design for an angle-of-attack range of - 8 ̊to 90 ̊/
- The boundary layer on compressor cascade blades
- The boundary layer on compressor cascade blades
- The boundary layer on compressor cascade blades
- The three-dimensional flow past a rapidly rotating circular cylinder
- Turbulent flow in a 180 ̊bend : modeling and computations
- Unstructured and adaptive mesh generation for high Reynolds number viscous flows
- Velocity-pressure integrated versus penalty finite element methods for high Reynolds number flows
- Wall-layer eruptions in turbulent flows

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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.library.in.gov/resource/o8b0WhBELwI/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/o8b0WhBELwI/">Reynolds number</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>

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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.library.in.gov/resource/o8b0WhBELwI/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/o8b0WhBELwI/">Reynolds number</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>`