Separated flow
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The concept Separated flow represents the subject, aboutness, idea or notion of resources found in San Francisco Public Library.
The Resource
Separated flow
Resource Information
The concept Separated flow represents the subject, aboutness, idea or notion of resources found in San Francisco Public Library.
- Label
- Separated flow
- Source
- nasat
20 Items that share the Concept Separated flow
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- Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight
- A computational study for the utilization of jet pulsations in gas turbine film cooling and flow control
- A computational study of multiple jet and wall interaction
- Active control of flow separation over an airfoil
- An experimental study of a separated/reattached flow behind a backward-facing step. Re[subscript h] = 37,000
- Computational fluid mechanics : progress report no. 18
- Computational study of separating flow in a planar subsonic diffuser
- Development of an actuator for flow control utilizing detonation
- Development of an axisymmetric afterbody test case for turbulent flow separation validation
- Experimental investigation of unsteady flows at large incidence angles in a linear oscillating cascade
- Exploring a method for improving turbulent separated-flow predictions with [k-omega] models
- In-flight flow visualization results from the X-29A aircraft at high angles of attack
- Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport
- Large eddy simulation of transonic flow field in NASA rotor 37
- Numerical study of three-dimensional separation and flow control at a wing-body junction : progress report for the period ended April 30, 1989
- Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration
- Summary of EASM turbulence models in CFL3D with validation test cases
- Supersonic retropropulsion test 1853 in NASA LaRC Unitary Plan Wind Tunnel test section 2
- The structure of dilute combusting sprays
- Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
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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.sfpl.org/resource/-KK5dokVRKk/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.sfpl.org/resource/-KK5dokVRKk/">Separated flow</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.sfpl.org/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="https://link.sfpl.org/">San Francisco Public 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.sfpl.org/resource/-KK5dokVRKk/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.sfpl.org/resource/-KK5dokVRKk/">Separated flow</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.sfpl.org/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="https://link.sfpl.org/">San Francisco Public Library</a></span></span></span></span></div>
