#
Separated flow
Resource Information
The concept ** Separated flow** represents the subject, aboutness, idea or notion of resources found in **Houston Public Library**.

The Resource
Separated flow
Resource Information

The concept

**Separated flow**represents the subject, aboutness, idea or notion of resources found in**Houston Public Library**.- Label
- Separated flow

- Source
- nasat

## Context

Context of Separated flow#### Subject of

- A comparative study of some dynamic stall models
- 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
- A computionally efficient modelling of laminar separation bubbles : semi-annual status report, June 1988 - January 1989 for NASA grant NAG-1-778
- A final report on the NASA grant NAG-1-1612 of large-vortex capture by a wing at very high angles of attack
- A numerical analysis applied to high angle of attack three-dimensional inlets
- A realizable Reynolds stress algebraic equation model
- A review of high-speed, convective, heat-transfer computation methods
- A steadying effect of acoustic excitation on transitory stall
- A study of the second and third order closure models of turbulence for prediction of separated shear flows
- A transport model of the turbulent scalar-velocity : status report
- A turbulence model for the NPARC code
- ALESEP, Part II : a computer program for the analysis of leading edge separation bubbles on infinite swept wings
- 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
- An experimental study of a separated/reattached flow behind a backward-facing step. Re[subscript h] = 37,000
- An experimental study of a turbulent boundary layer in the trailing edge region of a circulation-control airfoil
- An investigation of bleed configurations and their effect on shock wave/boundary layer interactions : final report
- Analysis of aerospike plume induced base-heating environment
- Analysis of transitional separation bubbles on infinite swept wings
- Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows
- Application of viscous-inviscid interaction methods to transonic turbulent flows
- Assessment of an unstructured-grid method for predicting 3-D turbulent viscous flows : 34th Aerospace Sciences Meeting, January 15-18, 1996/Reno, Nevada
- Boundary layer transition studies : November 1990 to February 1995
- Closed-loop separation control using oscillatory flow excitation
- Computation of separated and unsteady flows with one- and two-equation turbulence models : 32nd Aerospace Sciences meeting & exhibit, January 10-13, 1994/Reno, NV
- Computational fluid mechanics : progress report no. 18
- Computational study of separating flow in a planar subsonic diffuser
- Control of flow separation and mixing by aerodynamic excitation
- Control of low-speed turbulent separated flow over a backward-facing ramp
- Control of separated flow past a cylinder using tangential wall jet blowing
- Control of unsteady separated flow associated with the dynamic stall of airfoils
- Development of an actuator for flow control utilizing detonation
- Development of an axisymmetric afterbody test case for turbulent flow separation validation
- Effect of a rotating propeller on the separation angle of attack and distortion in ducted propeller inlets
- Effect of turbulence models on two massively-separated benchmark flow cases
- Enhanced design of turbo-jet LPT by separation control using phased plasma actuators
- Enhanced line integral convolution with flow feature detection : NAS technical report NAS-96-007
- Evaluation of F/A-18A HARV inlet flow analysis with flight data
- Evaluation of turbulence models for unsteady flows of an oscillating airfoil
- Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil
- Experimental investigation of plume-induced flow separation on the National Launch System 11/2-stage launch vehicle : 32nd Aerospace Sciences meeting & exhibit, January 10-13, 1994, Reno, NV
- Experimental investigation of unsteady flows at large incidence angles in a linear oscillating cascade
- Experimental investigation of unsteady flows at large incidence angles in a linear oscillating cascade
- Experimental parametric study of jet vortex generators for flow separation control
- Exploring a method for improving turbulent separated-flow predictions with [k-omega] models
- Final report on study of organized structures in the post-stall flow over wings
- Flow processes in overexpanded chemical rocket nozzles, Part 1, Flow separation
- Flow processes in overexpanded chemical rocket nozzles, Part 2, Side loads due to asymmetric separation
- Formation of asymmetric separated flow past slender bodies of revolution at large angles of attack
- Implementation of a two-equation K-[omega] turbulence model in NPARC
- 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
- Navier-Stokes analysis of turbine blade heat transfer
- Numerical investigation of separated transonic turbulent flows with a multiple-time-scale turbulence model
- Numerical investigation of the effects of icing on fixed and rotary wing aircraft : progress report for the period January 1, 1992-June 30, 1992
- Numerical simulation of helicopter engine plume in forward flight : final report cooperative agreement #NCC2-5061
- Numerical simulation of the SOFIA flowfield
- Numerical study of three-dimensional separation and flow control at a wing-body junction : progress report for the period ended April 30, 1989
- On the flow processes in sharply inclined and stalled airfoils in parallel movement and rotation
- PARC3D calculations of the F/A-18A HARV inlet vortex generators
- Physics of forced unsteady separation : proceedings of a NASA/AFOSR/ARO workshop held at NASA Ames Research Center, Moffett Field, California, April 17-19, 1990
- Prediction of the structure of fuel sprays in gas turbine combustors
- SSME main combustion chamber and nozzle flowfield analysis : final report
- Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6
- Simulation of brush insert for leading-edge-passage convective heat transfer
- Stability of a non-orthagonal stagnation flow to three dimensional disturbances
- Study of boundary layer development in a two-stage low-pressure turbine
- Study of the application of separation control by unsteady excitation to civil transport aircraft
- Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration
- 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
- 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
- The structure of dilute combusting sprays
- The structure of separated flow regions occurring near the leading edge of airfoils, including transition : semi-annual status report, February 1986-July 1986
- Third-moment closure of turbulence for predictions of separating and reattaching shear flows : final report on "A study of Reynolds-Stress Closure Model"
- Transient growth theory prediction of optimal placing of passive and active flow control devices for separation delay in LPT airfoils
- Transonic separated flow predictions based on a mathematically simple, nonequilibrium turbulence closure model
- Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
- Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
- Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method : EUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, GĂ¶ttingen, Germany, September 16-18, 1996
- Turbulence modeling
- Unsteady three-dimensional flow separation
- Unsteady three-dimensional marginal separation, including breakdown
- Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight
- Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight
- Vacuum chamber pressure effects on thrust measurements of low Reynolds number nozzles

## 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/-KK5dokVRKk/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.houstonlibrary.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.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 Separated flow

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/-KK5dokVRKk/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.houstonlibrary.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.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>`