Vortex-motion
Resource Information
The concept Vortex-motion represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
The Resource
Vortex-motion
Resource Information
The concept Vortex-motion represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
- Label
- Vortex-motion
- Authority link
- (EG-IN)672074
119 Items that share the Concept Vortex-motion
Context
Context of Vortex-motionSubject of
No resources found
No enriched resources found
- Wind tunnel investigation of vortex flows on F/A-18 configuration at subsonic through transonic speeds
- A comparison of airborne wake vortex detection measurements with values predicted from potential theory
- A computer code for gas-liquid two-phase vortex motions : GLVM
- A distributed vortex method for computing the vortex field of a missile
- A method for computing the leading-edge suction in a higher-order panel method
- A numerical study of three-dimensional vortex breakdown
- A study of streamwise vorticity-stirred combustion
- A study of the temporal stability of multiple cell vortices
- A vorticity dynamics based model for the turbulent dissipation : model development and validation
- A water tunnel flow visualization study of the vortex flow structures on the F/A-18 aircraft
- Aerodynamic properties of turbulent combustion fields
- Airfoil interaction with an impinging vortex
- Alton Pumping Station, Alton, Illinois : hydraulic model investigation
- An experimental analysis of critical factors involved in the breakdown process of leading edge vortex flows
- An experimental investigation of a turbulent junction vortex
- An experimental investigation of the chopping of helicopter main rotor tip vortices by the tail rotor
- Analysis and control of asymmetric vortex flows and supersonic vortex breakdown
- Analysis and control of asymmetric vortex flows and supersonic vortex breakdown : final report for the period December 1, 1991 to November 30, 1992
- Analysis and control of supersonic vortex breakdown flows
- Analysis of selected problems involving vortical flows
- Analytical studies of separated vortex flow on highly swept wings
- Analytical study of the origin and behavior of asymmetric vortices
- Application of a panel method to wake-vortex/wing interaction and comparison with experimental data
- Breakdown of Karman vortex street due to forced convection and flow compressibility
- Burst vortex/boundary layer interaction
- Calculation of symmetric and asymmetric votex separation on cones and tangent Ogives bases on discrete vortex models
- Calculations of axisymmetric vortex sheet roll-up using a panel and a filament model
- Characteristics of wake vortex generated by a Boeing 727 jet transport during two-segment and normal ILS approach flight paths
- Computation of design parameters and visualization of Goertler vortices : by Alok K. Verma, principal investigator
- Computation of potential flows with embedded vortex rings and applications to helicopter rotor wakes
- Control of vortical separation on conical bodies
- Controlled vortical flow on delta wings through unsteady leading edge blowing
- Crossflow effects on the growth rate of inviscid Görtler vortices in a hypersonic boundary layer
- Definition of the unsteady vortex flow over a wing/body configuration : final technical report, May 21-November 20, 1991
- Development of a perturbation generator for vortex stability studies
- Doppler acoustic vortex sensing system
- Effects of Görtler vortices, wall cooling and gas dissociation on the Rayleigh instability in a hypersonic boundary layer
- Effects of fog droplets on wake vortex decay rate
- Experimental and analytical study of the longitudinal aerodynamic characteristics of analytically and empirically designed strake-wing configurations at subcritical speeds
- Experimental investigation of the subwing tip and its vortex structure
- Exploratory wind-tunnel investigation of a wingtip-mounted vortex turbine for vortex energy recovery
- Feasibility of an onboard wake vortex avoidance system
- Flow visualization of the wake of a transport aircraft model with lateral-control oscillations
- Flow visualization study of a vortex/wing interaction
- Free vorticity field-boundary layer conversions : effect of boundary configuration and scale : progress report for NASA Langley Research Center
- Görtler vortices in growing boundary layers : the leading edge receptivity problem, linear growth and the nonlinear breakdown stage
- High angle-of-attack aerodynamic characteristics of crescent and elliptic wings
- Ignition and structure of a laminar diffusion flame in the field of a vortex
- In-flight leading-edge extension vortex flow-field survey measurements on a F-18 aircraft at high angle of attack
- Influence of large-scale motion on turbulent transport for confined coaxial jets
- Interaction between a vortex and a turbulent boundary layer, Part 1, Mean flow evolution and turbulence properties
- Interaction of two convective scales within a severe thunderstorm, case study : and Thunderstorm wake vortex structure and aerodynamic origin
- Investigation of stable atmospheric stratification effect on the dynamics of descending vortex pairs
- Inviscid vortex motions in weakly three-dimensional boundary layers and their relation with instabilities in stratified shear flows
- Joint US/UK vortex tracking program at Heathrow International Airport
- Localized and distributed boundary-layer receptivity to convected unsteady wake in free stream
- Low-speed wind-tunnel parametric investigation of flight spoilers as trailing-vortex-alleviation devices on a transport aircraft model
- Measurement of the trailing vortex systems of large transport aircraft, using tower fly-by and flow visulization : (summarly, comparison and application)
- Measurement of vortex flow fields
- Motion and interaction of decaying trailing vortices in spanwise shear wind
- Nonsteady Laboratory simulation of atmospheric vortices : inertial oscillations and tornado skip
- Numerical study of the trailing vortex of a wing with wing-tip blowing
- On nonlinear Tollmien-Schlichting/vortex interaction in three dimensional boundary layers
- On the effects of viscosity on the stability of a trailing-line vortex
- On the initial stages of vortex wave interactions in highly curved boundary layer flows
- On the instability of Görtler vortices to nonlinear travelling waves
- On the receptivity problem for 0 (1) wavelength
- On the receptivity problem for Görtler vortices : vortex motions induced by wall roughness
- On the secondary instability of the most dangerous Görtler vortex
- On the spatial evolution of long-wavelength Görtler vortices governed by a viscous inviscid interaction, Part I | The Linear case
- On the stabliity of nonlinear viscous vortices in three-dimensional boundary layers
- On vortex bursting
- One-degree-of-freedom motion induced by modeled vortex shedding
- Perpendicular blade vortex interaction and its implications for helicopter noise prediction : final report to NASA Langley on research performed under grant NAG-1-1119, "wave-number frequency spectra in a trailing vortex for BSI noise prediction" for the period ending 15th August, 1993
- Prediction and control of vortex-dominated and vortex-wake flows
- Prediction of vortex shedding from circular and noncircular bodies in subsonic flow
- Prediction of vortex shedding from circular and noncircular bodies in supersonic flow
- Preliminary study of a wing-tip vortex using laser velocimetry
- Pulsed acoustic vortex sensing system
- Reduction in size and unsteadiness of a VTOL ground vortex by ground fences : final technical report
- Review of some vortex relations
- Role of acoustics in flame/vortex interactions
- Rotorcraft application of advanced computational aerodynamics
- Safety issues related to wake vortex encounters during visual approach to landing : special investigation report
- Semi-annual status report on NASA grant NSG 1629 "An investigation of vortex-induced aerodynamic characteristics of supersonic cruise configurations" : July 1, 1984 - December 31, 1984
- Semi-annual status report on research grant no. NAGW-581 Vortex boundary-layer interactions, period 1 March 1986 - 31 August 1986
- Semiempirical method for predicting vortex-induced rolling moments
- Specification for a Program for an Interative Aeroelastic Solution (PIAS)
- Stability of fluid flow in a cylindrical annulus
- Supersonic mixing enhancement by vorticity for high-speed propulsion : final report for the period April 1, 1988 - June 30, 1991
- Supersonic shock wave/vortex interaction
- The Görtler vortex instability mechanism in three-dimensional boundary layers
- The development of a mixing layer under the action of weak streamwise vortices
- The ground vortex flowfield associated with a jet in a cross flow impinging on a ground plane for uniform and annular turbulent axisymmetric jets
- The growth of Goertler vortices in compressible boundary layers
- The inviscid secondary instability of fully nonlinear longitudinal vortex structures in growing boundary layers
- The measurement of the Boeing 707 trailing vortex system using the tower fly-by technique
- The stability of a trailing-line vortex in compressible flow
- Three-dimensional simulation of vortex breakdown
- Tip vortices of wings in subsonic and transonic flow : a numerical simulation
- Underwing compression vortex attenution device
- Unsteady stagnation-point heat transfer during passage of a concentrated vortex
- User's guide, tip vortex computer code, SRATIP
- VORCOR : a computer program for calculating characteristics of wings with edge vortex separation by using a vortex filament and core model
- Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel
- Visualization of leading edge vortices on a series of flat plate delta wings
- Vortex advisory system safety analysis
- Vortex boundary-layer interactions, data report : semiannual status report on research grant no. NAGW-581, period 1 March 1985 - 31 August 1985
- Vortex breakdown and control experiments in the Ames-Dryden water tunnel
- Vortex characteristics of C5A/B, C141B and C130E aircraft applicable to ATC terminal flight operations tower fly-by data
- Vortex characteristics of C5A/B, C141B, and C130E aircraft applicable to ATC terminal flight operations tower fly-by data
- Vortex generation and wave-vortex interaction over a concave plate with roughness and suction
- Vortex interactions and decay in aircraft wakes
- Vortex wake alleviation studies with a variable twist wing
- Vortex wake characteristics of B757-200 and B767-200 aircraft using the tower fly-by technique
- Vortex/boundary-layer interactions, data report : final report on NASA grant NAGw-581
- Vortex/boundary-layer interactions, data report : final report on NASA grant NAGw-581 / A.D. Cutler and P. Bradshaw
- Wake vortex separation standards : analysis methods : final report
- Water-tunnel experiments on an oscillating airfoil at RE = 21,000
- Wind tunnel investigation of the interaction and breakdown characteristics of slender-wing vortices at subsonic, transonic, and supersonic speeds
Embed
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.library.in.gov/resource/AebE4br3Vrk/" 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/AebE4br3Vrk/">Vortex-motion</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>
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 Vortex-motion
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.library.in.gov/resource/AebE4br3Vrk/" 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/AebE4br3Vrk/">Vortex-motion</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>
