Low Reynolds number
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The concept Low Reynolds number represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
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Low Reynolds number
Resource Information
The concept Low Reynolds number represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
- Label
- Low Reynolds number
- Source
- nasat
21 Items that share the Concept Low Reynolds number
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- Validation of a CFD methodology for variable speed power turbine relevant conditions
- A computational study for the utilization of jet pulsations in gas turbine film cooling and flow control
- A k-E [i.e. Kappa-Epsilon] calculation of transitional boundary layers
- An evaluation of three two-dimensional computational fluid dynamics codes including low Reynolds numbers and transonic Mach numbers
- Assessment of aerodynamic challenges of a variable-speed power turbine for large civil tilt-rotor application
- CMOTT turbulence module for NPARC : under cooperative agreement NCC3-520
- Computational work to support FAP/SRW variable-speed power-turbine development
- Design and performance calculations of a propeller for very high altitude flight
- Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment
- Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment
- Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations : a final technical report for NASA-LeRC grant NAG-1781
- Dynamic wind-tunnel testing of a sub-scale iced S-3B Viking
- Efficient parallel algorithm for direct numerical simulation of turbulent flows
- Ice accretions and full-scale iced aerodynamic performance data for a two-dimensional NACA 23012 airfoil
- Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade
- Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure
- Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure
- Mars science helicopter conceptual design
- Requirements for large eddy simulation computations of variable-speed power turbine flows
- Slip-boundary equations for multicomponent nonequilibrium airflow
- The screem-J4D : a proposal in response to a low Reynolds number station keeping mission
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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.umsl.edu/resource/GvgLefcerCw/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/GvgLefcerCw/">Low Reynolds number</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>
