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

The Resource
Vortices
Resource Information

The concept

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

- Source
- nasat

## Context

Context of Vortices#### Subject of

- A candidate wake vortex strength definition for application to the NASA Aircraft Vortex Spacing System (AVOSS)
- A candidate wake vortex strength definition for application to the NASA Aircraft Vortex Spacing System (AVOSS)
- A coupled Eulerian/Lagrangian method for the solution of three-dimensional vortical flows
- A coupled probabilistic wake vortex and aircraft response prediction model
- A final report on the NASA grant NAG-1-1612 of large-vortex capture by a wing at very high angles of attack
- A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines
- A new methodology for free wake analysis using curved vortex elements
- A note on trapping moving vortices
- A numerical model of unsteady, subsonic aeroelastic behavior
- A numerical model of unsteady, subsonic aeroelastic behavior
- A parametric study of accelerations of an airplane due to a wake vortex system
- A parametric study of accelerations of an airplane due to a wake vortex system
- A parametric study of transonic blade-vortex interaction noise
- A predictor-corrector scheme for vortex identification
- A predictor-corrector technique for visualizing unsteady flow
- A smoke generator system for aerodynamic flight research
- A study of Dean vortex development and structure in a curved rectangular channel with aspect ratio of 40 at Dean numbers up to 430
- A study of the factors affecting boundary layer two-dimensionality in wind tunnels
- A study of the temporal stability of multiple cell vortices
- A study of the vortex flow over 76/40-deg double-delta wing
- A three-dimensional CFD investigation of secondary flow in an accelerating, 90 ̊elbow
- A three-dimensional dual potential procedure with applications to wind tunnel inlets and interacting boundary layers : final report
- A time-accurate adaptive grid method and the numerical simulation of shock-vortex interaction
- A viscous-inviscid interactive procedure for rotational flow in cascades of two dimensional airfoils of arbitrary shape : final report
- A wind tunnel investigation of the effects of micro-vortex generators and Gurney flaps on the high-lift characteristics of a business jet wing
- Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications : final report for the period December 1, 1995 through Novemeber 30, 1996
- Airfoil dynamic stall and rotorcraft maneuverability
- Airfoil dynamic stall and rotorcraft maneuverability
- An analysis of blade vortex interaction aerodynamics and acoustics
- An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet
- An assessment of 3-C PIV analysis methodology for HART II measured data
- An assessment of viscous effects in computational simulation of benign and burst vortex flows on generic fighter wind-tunnel models using TEAM code
- An experimental investigation of the ground vortex created by a moving jet
- An exploratory study of apex fence flaps on a 74-degree delta wing
- An operational computational Terminal Area PBL Prediction System : NASA grant NCC-1-220, calendar year 97 annual report
- Analytical investigation of rotor wake formation and geometry : progress report for NASA grant NAG-2-275 for period April 15, 1985 - October 15, 1985
- Analytical study of the origin and behavior of asymmetric vortices
- Application of particle image velocimetry to a study of flow about a multi-element airfoil : final report for the period August 15, 1995 to August 14, 1996 ... grant no. NCC2-5155
- Application of wind tunnel free-flight technique for wake vortex encounters
- Bellows flow-induced vibrations
- Boundary layer flow control by an array of ramp-shaped vortex generators
- Calculated low-speed steady and time-dependent aerodynamic derivatives for some airfoils using a discrete vortex method
- Characteristic eddy decomposition of turbulence in a channel
- Characterizing the wake vortex signature for an active line of sight remote sensor
- Compressible flows with periodic vortical disturbances around lifting airfoils
- Computation of asymmetric supersonic flows around cones at large incidence : final report
- Computational methods for the problems of the tip vortex : final technical report
- Concerning the interaction of non-stationary cross-flow vortices in a three-dimensional boundary layer
- Control of low-speed turbulent separated flow over a backward-facing ramp
- Convection of a pattern of vorticity through a reacting shock wave
- Deflected jet experiments in a turbulent combustor flowfield
- Design and integration of an actuated nose strake control system
- Detailed flow-field measurements over a 75° swept delta wing
- Development of a mulicomponent force and moment balance for water tunnel applications
- Devices that alter the tip vortex of a rotor
- Discrete-vortex model for the symmetric-vortex flow on cones
- Documentation of atmospheric conditions during observed rising aircraft wakes
- Double-branched vortex generator
- Effect of a rotor wake on the local heat transfer on the forward half of a circular cylinder
- Enhanced mixing of an axisymmetric jet by aerodynamic excitation
- Euler technology assessment for preliminary aircraft design employing OVERFLOW code with multiblock structured-grid method
- Evaluation of F/A-18A HARV inlet flow analysis with flight data
- Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
- Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor
- Experimental blade vortex interaction noise characteristics of a utility helicopter at 1/4 scale
- Experimental investigation of the low NOx vortex airblast annular combustor
- Experimental results of the control of a vortical flow by tangential blowing
- Experimental studies of vortex flows : final report, NASA grant NCC 2-294, report covering the period March 1984 - May 1988
- Experimental study of complex vortex interactions in the wake of high aspect ratio wings : final report on NASA grant NAG-1-1816
- Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges
- Experiments in aircraft roll-yaw control using forebody tangential blowing
- F/A-18 forebody vortex control
- Fan noise reduction achieved by removing tip flow irregularities behind the rotor--forward arc test configuration
- Far-field turbulent vortex-wake/exhaust plume interaction for subsonic and HSCT airplanes : 27th AIAA Fluid Dynamics Conference, June 17-20, 1996/New Orleans, LA
- Feasibility of generating an "artificial" burst in a turbulent boundary layer
- Flow in serpentine coolant passages with trip strips : technical progress narrative report, reporting period September 1, 1995 to September 30, 1995
- Flow past a flat plate with a vortex/sink combination
- Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model
- Flutter clearance flight tests of an OV-10A airplane modified for wake vortex flight experiments
- Formal optimization of hovering performance using free wake lifting surface theory
- Formation of asymmetric separated flow past slender bodies of revolution at large angles of attack
- Helicopter model rotor-blade vortex interaction impulsive noise : scalability and parametric variations
- Helicopter tail rotor noise analyses : final technical report ; period, June 1, 1985 - January 31, 1986
- Hopf bifurcation in the driven cavity
- Ignition dynamics of a laminar diffusion flame in the field of a vortex embedded in a shear flow
- Implementation and validation of a wake model for vortex-surface interactions in low-speed forward flight : semi-annual status report, period 10/1/86 - 3/31/87
- Indicial response approach derived from Navier-Stokes equations, Part 1, Time-invariant equilibrium state
- Initial circulation and peak vorticity behavior of vortices shed from airfoil vortex generators
- Initialization and simulation of three-dimensional aircraft wake vortices : final report for the period ending May 1997, under grant# NAG-1-1437
- Instabilities and and subharmonic resonances in subsonic heated round jets
- Instabilities originating from suction holes used for laminar flow control (LFC)
- Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study
- Interaction of a shock with a longitudinal vortex
- LES, DNS, and RANS for the analysis of high-speed turbulent reacting flows : annual report submitted to NASA Langley Research Center : progress report ... under grant NAG 1-1122 for the period August 1, 1995 - July 31, 1996
- Large-eddy/Lattice Boltzmann simulations of micro-blowing strategies for subsonic and supersonic drag control
- Large-scale advanced propeller blade pressure distributions : predictions and data
- Lee-side flow over delta wings at supersonic speeds
- Linear instability of a uni-directional transversely sheared mean flow
- Low speed aerodynamics of the X-38 CRV : final report, E16-N63
- Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing
- Measured changes in C-band radar reflectivity of clear air caused by aircraft wake vortices
- Measurements and modeling of flow structure in the wake of a low profile "wishbone" vortex generator
- Measurements of a turbulent horseshoe vortex formed around a cylinder
- Measurements of wing-tip blowing
- Method of measuring cross-flow vortices by use of an array of hot-film sensors
- Modeling of vortex-induced oscillations based on indicial response approach
- NACA 0015 wing pressure and trailing vortex measurements
- Navier-Stokes flow field analysis of compressible flow in a high pressure safety relief valve
- Navier-Stokes simulation of several high-lift reference H configurations
- Navier-Stokes, flight, and wind tunnel flow analysis for the F/A-18 aircraft
- Near-planar TS waves and longitudinal vortices in channel flow : nonlinear interaction and focusing
- Nonlinear Tollmien-Schlichting/vortex interaction in boundary layers
- Nonlinear stability of non-stationary cross-flow vortices in compressible boundary layers
- Numerical modeling studies of wake vortex transport and evolution within the planetary boundary layer : NASA grant NCC-1-188 : FY 97 annual report
- Numerical simulation of Gortler/Tollmien-Schlichting wave-interaction
- Numerical simulation of the flow about the F-18 HARV at high angle of attack
- Numerical simulation of two-dimensional, spatially developing mixing layers
- Numerical solutions of the complete Navier-Stokes equations : progress report no. 27 for the period October 1, 1995 to September 30, 1996
- Nummerical studies of interacting vortices
- Observed changes in atmospheric boundary layer properties at Memphis International Airport during August 1995
- On multiple-layered vortices
- On the Görtler instability in hypersonic flows : Sutherland law fluids and real gas effects
- On the consistency of Reynolds stress turbulence closures with hydrodynamic stability theory
- On the generation of mean flows by the interaction of Görtler vortices and Tollmien-Schlichting waves in curved channel flows
- On the nonlinear evolution of a stationary cross-flow vortex in a fully three-dimensional boundary layer flow
- Operational performance of vapor-screen systems for in-flight visualization of leading-edge vortices on the F-106B aircraft
- Overview of HATP experimental aerodynamics data for the baseline F/A-18 configuration : High-Angle-of-Attack Technology Conference
- Overview of the preparation and use of an OV-10 aircraft for wake vortex hazards flight experiments
- Potential impacts of advanced aerodynamic technology on air transportation system productivity
- Prediction and control of vortex-dominated and vortex-wake flows : final report for the period December 1, 1993 through December 1, 1995
- Preliminary study of a model rotor in descent
- Preprocessing for eddy dissipation rate and TKE profile generation
- Pressure measurements of impinging jet with asymmetric nozzle : progress report
- Proceedings of the NASA First Wake Vortex Dynamic Spacing Workshop : proceedings of a workshop sponsored by the National Aeronautics and Space Administration, Washington, D.C., and held at Langley Research Center, Hampton, Virginia, May 13-15, 1997
- Radar reflectivity in wingtip-generated wake vortices
- Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate) : final report of TsAGI under cooperative agreement # NCCW-72
- Results of the integration of a transonic full-potential analysis program with a free-wake lifting-line program for hovering rotors
- Second order modeling of boundary-free turbulent shear flows
- Secondary instability of stationary crossflow vortices in Mach 6 boundary layer over a circular cone
- Self-similar compressible free vortices
- Semiempirical method for predicting vortex-induced rolling moments
- Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters
- Shear layer excitation, experiment versus theory
- Simulating wake vortex detection with the Sensivu Doppler wind lidar simulator
- Simultaneous three-dimensional velocity and mixing measurments by use of laser Doppler velocimetry and fluorescence probes in a water tunnel
- Some design philosophy for reducing the community noise of advanced counter-rotation propellers
- Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails : 36th Aerospace Sciences meeting & exhibit : January 12-15, 1998/Reno, NV
- Spreading characteristics and thrust of jets from asymmetric nozzles
- Stereo-video data reduction of wake vortices and trailing aircrafts
- Study for prediction of rotor/wake/fuselage interference
- Study of the mutual interaction between a wing wake and an encountering airplane : NASA grant no. NAG1-1572, final report
- Subsonic aerodynamic assessment of vortex flow management devices on a high-speed civil transport configuration
- Subsonic flow investigations on a cranked wing designed for high maneuverability
- 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 in-flight flow visualization obtained from the NASA high alpha research vehicle
- System identification of a vortex lattice aerodynamic model
- The F/A-18 high-angle-of-attack ground-to-flight correlation, lessons learned
- The aerodynamic characteristics of vortex ingestion for the F/A-18 inlet duct
- The atmospheric effects of stratospheric aircraft : a fourth program report
- The decay of longitudinal vortices shed from airfoil vortex generators
- The dissipation range in rotating turbulence
- The effect of crossflow on Görtler vortices
- The effects of viscosity on the stability of a trailing-line vortex in compressible flow
- The effects of vortex ingestion on the flow in a diffusing S-DUCT
- The fully nonlinear development of Görtler vortices in growing boundary layers
- The nonlinear evolution of inviscid Gortler vortices in three-dimensional boundary layers
- The thermal-vortex equations : final report
- The thermal-vortex equations : final report
- Theoretical and experimental investigation of vortex breakdown : final technical report, June 1, 1985 - May 31, 1986
- Theoretical studies on flapped delta wings
- Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators
- Three-centimeter Doppler radar observations of wingtip-generated wake vortices in clear air : under contract NAS1-18925
- Toward the large-eddy simulations of compressible turbulent flows
- Tracking a turbulent spot in an immersive environment
- Transition to turbulence in plane channel flow
- Transonic Navier-Stokes calculations about a 65° delta wing
- Transonic interaction of unsteady vortical flows
- Transverse vorticity measurements using an array of four hot-wire probes
- Turbulence measurements in the near field of a wingtip vortex
- Turbulence measurements in the near field of a wingtip vortex
- Turbulence structures associated with the bursting event
- VORSTAB, a computer program for calculating lateral-directional stability derivatives with vortex flow effect
- Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel
- Vertical tail buffeting alleviation using piezoelectric actuators : some results of the Actively Controlled Response of Buffet-Affected Tails (ACROBAT) program
- Video photographic considerations for measuring the proximity of a probe aircraft with a smoke seeded trailing vortex
- Viscous flows in rotating pipes with internal cavities and related vortex breakdowns
- Viscous wing theory development : final report
- Visualizing time-varying phenomena in numerical simulations of unsteady flows
- Vortex breakdown incipience : theoretical considerations
- Vortex conception of rotor and mutual effect of screw/propellers
- Vortex generating flow passage design for increased film-cooling effectiveness and surface coverage
- Vortex instabilities in 3D boundary layers : the relationship between Görtler and crossflow vortices
- Vortex interaction with a leading-edge of finite thickness
- Vortex perturbation dynamics
- Vortex systems on slender rotating bodies and their effect on the aerodynamic coefficients
- Vortex tubes in turbulent flows : identification, representation, reconstruction
- Vortex/body interaction and sound generation in low-speed flow
- Vortex/body interaction and sound generation in low-speed flow
- Vortex/boundary-layer interaction : semi-annual status report on research grant no. NAGW-581
- Vortical dissipation in two-dimensional shear flows
- Wake geometry measurements and analytical calculations on a small-scale rotor model
- Wake vortex advisory system (Wake VAS) concept of operations
- Wake vortex field measurement program at Memphis, Tennessee : data guide
- Water tunnel flow visualization study of a 4.4% scale X-31 forebody
- Wavenumber selection for small-wavelength Görtler vortices in curved channel flows
- Weakly nonparallel and curvature effects on stationary crossflow instability : comparison of results from multiple-scales analysis and parabolized stability equations
- Wind tunnel investigation of passive porosity applied to the leading-edge extension and leading-edge flaps on a slender wing at subsonic speed
- Wind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds

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