Reynolds number
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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
66 Items that share the Concept Reynolds number
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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>
