#
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

## Context

Context of Reynolds number#### Subject of

- A finite Reynolds number approach for the prediction of boundary layer receptivity in localized regions
- 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
- 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
- Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes
- An efficient and robust algorithm for two dimensional time dependent incompressible Navier-Stokes equations : high Reynolds number flows
- 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 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 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 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 cast 10-2/DOA 2 airfoil in the Langley 0.3-meter transonic cryogenic tunnel - phase II
- Highlights of unsteady pressure tests on a 14 percent supercritical airfoil at high Reynolds number, transonic condition
- Hot-jet simulation in cryogenic wind tunnels
- 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
- 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
- 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
- Unstructured and adaptive mesh generation for high Reynolds number viscous flows
- Water-tunnel study of transition flow around circular cylinders

## Embed (Experimental)

### Settings

Select options that apply then copy and paste the RDF/HTML data fragment to include in your application

Embed this data in a secure (HTTPS) page:

Layout options:

Include data citation:

<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.houstonlibrary.org/resource/dGadqAc-fJQ/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.houstonlibrary.org/resource/dGadqAc-fJQ/">Reynolds number</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.houstonlibrary.org/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.houstonlibrary.org/">Houston Public Library</a></span></span></span></span></div>

Note: Adjust the width and height settings defined in the RDF/HTML code fragment to best match your requirements

### Preview

## Cite Data - Experimental

### Data Citation of the Concept Reynolds number

Copy and paste the following RDF/HTML data fragment to cite this resource

`<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.houstonlibrary.org/resource/dGadqAc-fJQ/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.houstonlibrary.org/resource/dGadqAc-fJQ/">Reynolds number</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.houstonlibrary.org/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.houstonlibrary.org/">Houston Public Library</a></span></span></span></span></div>`