Wind tunnels
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The concept Wind tunnels represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
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Wind tunnels
Resource Information
The concept Wind tunnels represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
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- Wind tunnels
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- (EG-IN)676479
240 Items that share the Concept Wind tunnels
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- X-29A longitudinal and directional force and moment supplemental transonic wind tunnel test results
- A Laser velocimeter system for large-scale aerodynamic testing
- A Lumped parameter mathematical model for simulation of subsonic wind tunnels
- A New design concept for indraft wind-tunnel inlets with application to the national full-scale aerodynamic complex
- A critical assessment of wind tunnel results for the NACA 0012 airfoil
- A linearly controlled direct-current power source for high-current inductive loads in a magnetic suspension wind tunnel
- A method for modifying two-dimensional adaptive wind-tunnel walls including analytical and experimental verification
- A numerical simulation of the NFAC (National Full-Scale Aerodynamics Complex) open-return wind tunnel inlet flow
- A numerical study of the effects of wind tunnel wall proximity on an airfoil model
- A quiet flow Ludwieg tube for study of transition in compressible boundary layers : design and feasibility
- A quiet flow Ludwieg tube for study of transition in compressible boundary layers : design and feasibility
- A study of juncture flow in the NASA Langley 0.3-meter transonic cryogenic tunnel
- A swept wing panel in a low speed flexible walled test section
- A theoretical study of non-adiabatic surface effects for a model in the NTF cryogenic wind tunnel
- A tilting wind tunnel for fire behavior studies
- A voice-actuated wind tunnel model leak checking system
- A wind tunnel investigation of the Deer Isle-Sedgwick Bridge, phase I
- A wind-tunnel study of the applicability of far-field sonic-boom theory to the space shuttle orbiter
- Acoustical evaluation of the NASA Lewis 9- by 15-foot low speed wind tunnel
- Acquisition and utilization of wind tunnels by the National Aeronautics and Space Administration : report to the Committee on Science and Technology, House of Representatives
- Advanced recovery systems wind tunnel test report
- Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests)
- Aerodynamic characteristics of an air-exchanger system for the 40-by 80-foot wind tunnel at Ames Research Center
- Aerodynamic characteristics of the 40-by 80/80- by 120-foot wind tunnel at NASA Ames Research Center
- Aerodynamic characteristics of the modified 40- by 80-foot wind tunnel as measured in a 1/50th-scale model
- Aerodynamic design guidelines and computer program for estimation of subsonic wind tunnel performance
- Aerodynamic design of the contoured wind-tunnel liner for the NASA supercritical, laminar-flow-control, swept-wing experiment
- Aerodynamic force measurements with a strain-gage balance in a cryogenic wind tunnel
- Aerodynamic performance of the 17-M-diameter Darrieus wind turbine in the three-bladed configuration : an addendum
- Aerodynamic performance of the 17-metre-diameter Darrieus wind turbine
- Aeroelastic considerations for torsionally soft rotors
- Aerofoil testing in a self-streamlining flexible walled wind tunnel
- Aeronautical facilities assessment
- An analysis of sound absorbing linings for the interior of the NASA Ames 80x120-foot wind tunnel
- An evaluation in a modern wind tunnel of the transonic adaptive wall adjustment developed by NPL in the 1940's
- An evaluation of proposed acoustic treatments for the NASA LaRC 4 x 7 meter wind tunnel
- An experimental evaluation of advanced rotorcraft airfoils in the NASA Ames eleven-foot wind tunnel
- An experimental investigation of end treatments for nonreturn wind tunnels
- An integrated CFD/experimental analysis of aerodynamic forces and moments
- Analysis of 7- x 10-foot high speed wind tunnel shaft loads in support of fan blade failure investigation
- Analysis of open loop higher harmonic control at high airspeeds on a modern four-bladed articulated rotor
- Analysis of rotary balance data for the F-15 airplane including the effect of conformal fuel tanks
- Analytical and physical modeling program for the NASA Lewis Research Center's Altitude Wind Tunnel (AWT)
- Analytical modeling of circuit aerodynamics in the new NASA Lewis Altitude Wind Tunnel
- Application of fuzzy logic to the control of wind tunnel settling chamber temperature
- Application of laser velocimetry to unsteady flows in large scale high speed tunnels
- Application of two design methods for active flutter suppression and wind-tunnel test results
- Background noise measurements from jet exit vanes designed to reduce flow pulsations in an open-jet wind tunnel
- Calibration of transonic and supersonic wind tunnels
- Comparison of analytical and experimental performance of a wind-tunnel diffuser section
- Comparison of propeller cruise noise data taken in the NASA Lewis 8- by 6-foot wind tunnel with other tunnel and flight data
- Computer analysis of flow pertubations generated by placement of choke bumps in a wind tunnel
- Computer program for calculating flow parameters and power requirements for cryogenic wind tunnels
- Computer program for plotting and fairing wind tunnel data
- Configuration design studies and wind tunnel tests of an energy efficient transport with a high-aspect-ratio supercritical wing
- Considerations for the installation of honeycomb and screens to reduce wind-tunnel turbulence
- Cryogenic strain gage techniques used in force balance design for the National Transonic Facility
- Cryogenic wind technology : a way to measurement at higher Reynolds numbers
- Cryogenic wind tunnels : a selected, annotated bibliography
- Cryogenic wind tunnels : problems of continuous operation at low temperatures
- Current wind tunnel capability and planned improvements at Lewis Research Center
- Description and calibration of the Langley Unitary Plan Wind Tunnel
- Design and Navier-Stokes analysis of hypersonic wind tunnel nozzles
- Design and fabrication of forward-swept counterrotation blade configuration for wind tunnel testing : final report
- Design and performance of a fixed, nonaccelerating, guide vane cascade that operates over an inlet flow angle range of 600
- Design and wind tunnel evaluation of a symmetric airfoil series for large wind turbine applications
- Design features and operational characteristics of the Langley 0.3-meter transonic cryogenic tunnel
- Design study of test models of maneuvering aircraft configurations for the National Transonic Facility
- Design, test, and evaluation of three active flutter suppression controllers
- Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Researach Center's proposed altitude wind tunnel
- Development and application of dynamic simulations of a subsonic wind tunnel
- Development of a distributed-parameter mathematical model for simulation of cryogenic wind tunnels
- Development of microchannel plates in advanced wind-tunnel instrumentation
- Device for quick changeover between wind tunnel force and pressure testing : patent application
- Direct calculation of wall interferences and wall adaptation for two-dimensional flow in wind tunnels with closed walls
- Dynamic measurement of total temperature, pressure, and velocity in the Langley 0.3-meter transomic cryogenic tunnel
- Dynamic response characteristics of two transport models : tested in the National Transonic Facility
- Dynamic wind-tunnel tests of an aeromechanical gust-alleviation system using several different combinations of control surfaces
- Effect of jet exit vanes on flow pulsations in an open-jet wind tunnel
- Effect of wind tunnel acoustic modes on linear oscillating cascade aerodynamics
- Engineering changes to the 0.1m cryogenic wind tunnel at Southampton University
- Evaluation of a new concept for reducing free-stream turbulence in wind tunnels
- Evaluation of a quartz bourdon pressure gage for wind tunnel mach number control system application
- Evaluation of the Langley 4- by 7-meter tunnel for propeller noise measurements
- Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results
- Evaluation tests of platinum resistance thermometers for a cryogenic wind tunnel application
- Evolution, calibration, and operational characteristics of the two-dimensional test section of the Langley 0.3-meter transonic cryogenic tunnel
- Experimental evaluation of blockage ratio and plenum evacuation system flow effects on pressure distribution for bodies of revolution in 0.1-scale model test section of NASA Lewis Research Center's proposed altitude wind tunnel
- Experimental evaluation of corner turning vanes : summary
- Experimental evaluation of honeycomb/screen configurations and short contraction section for NASA Lewis Research Center's altitude wind tunnel
- Experimental evaluation of turning vane designs for high-speed and coupled fan-drive corners of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel
- Experimental evaluation of two turning vane designs for fan drive corner 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel
- Experimental evaluation of wall Mach number distributions of the octagonal test section proposed for NASA Lewis Research Center's altitude wind tunnel
- Experimental investigation of the subsonic high-altitude operation of the NASA Lewis 10- by 10-foot supersonic wind tunnel
- Experimental results for the Eppler 387 airfoil at low Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel
- Experimental studies of flow separation of three airfoils at low speeds
- Experimental study of an independently deflected wingtip mounted on a semispan wing
- Experimental validation study of an analytical model of discrete frequency sound propagation in closed-test-section wind tunnels
- Experiments in a three-dimensional adaptive-wall wind tunnel
- F-15 rotary balance data for an angle-of-attack range of 80 to 900
- Fastener load tests and retention systems tests for cryogenic wind-tunnel models
- Finite-rate water condensation in combustion-heated wind tunnels
- Flexwall : a computer program for predicting the wall modifications for two-dimensional, solid, adaptive-wall wind tunnels
- Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic mach numbers
- Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane
- Flow quality studies of the NASA Lewis Research Center 8- by 6-foot supersonic/9- by 15-foot low speed wind tunnel
- Flow quality studies of the NASA Lewis Research Center Icing Research Tunnel
- Flow quality studies of the NASA Lewis Research Center Icing Research Tunnel diffuser
- Flowfield measurements in the NASA Lewis Research Center 9- by 15-foot low-speed wind tunnel
- Further wind tunnel investigation of the SM701 airfoil with aileron and turbulators
- Heat transfer and pressure drop performance of a finned-tube heat exchanger proposed for use in the NASA Lewis altitude wind tunnel
- Heat transfer distributions around nominal ice accretion shapes formed on a cylinder in the NASA Lewis icing research tunnel
- Hot-jet simulation in cryogenic wind tunnels
- In-situ technique for checking the calibration of platinum resistance thermometers
- Initial investigation of cryogenic wind tunnel model filler materials
- Integral method of wall interference correction in low-speed wind tunnels
- Introduction to cryogenic wind tunnels
- Investigation of the asymmetric aerodynamic characteristics of cylindrical bodies of revolution with variations in nose geometry and rotational orientation at angles of attack to 58Ã¥nd Mach numbers to 2
- Investigation of the flow in the diffuser section of the NASA Lewis Icing Research Tunnel
- Investigation of very low blockage ratio boattail models in the Langley 16-foot transonic tunnel
- Iterative adaptation of the bidimensional wall of the French T2 wind tunnel around a C5 axisymmetrical model : infinite variation of the Mach number at zero incidence and a test at increased incidence
- J-85 jet engine noise measured in the ONERA S1 wind tunnel and extrapolated to far field
- KC-135 Winglet Program Review : proceedings of a symposium held at Dryden Flight Research Center, Edwards, California, September 16, 1981
- Laser velocimeter data aquisition system for the Langley 14- by 22-foot subsonic tunnel : software reference guide version 3.3
- Laser velocimetry in the low-speed wind tunnels at Ames Research Center
- Laser-velocimeter surveys of merging vortices in a wind tunnel : complete data and analysis
- Loads and performance data from a wind-tunnel test of model articulated helicopter rotors with two different blade torsional stiffnesses
- Longitudinal aerodynamic characteristics of an elliptical body with a horizontal tail at mach numbers 2.3 to 4.63
- Low-speed wind tunnel performance of high-speed counterrotation propellers at angle-of-attack
- Mean velocity, turbulence intensity and turbulence convection velocity measurements for a convergent nozzle in a free jet wind tunnel
- Methods for assessing wall interference in the 2- by 2-foot adaptive-wall wind tunnel
- Miniature remote dead weight calibrator : patent application
- Model representation in the PANCOR wall interference assessment code
- Model rotor icing tests in the NASA Lewis icing research tunnel
- Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment
- NASA Lewis 9-by 15-foot low-speed wind tunnel user manual
- NASA Lewis wind tunnel model systems criteria
- New coherent optical techniques for national transonic wind tunnel facility : final technical report
- Noise generated by flow through large butterfly valves
- Numerical study of the aerodynamic effects of using sulfur hexafluoride as a test gas in wind tunnels
- One-fiftieth scale model studies of 40- by 80-foot and 80- by 120-foot wind tunnel complex at NASA Ames Research Center
- Onset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel
- Overview of the Applied Aerodynamics Division
- Performance and test section flow characteristics of the National Full-Scale Aerodynamics Complex 40- by 80-Foot Wind Tunnel
- Performance and test section flow characteristics of the National Full-Scale Aerodynamics Complex 80- by 120-Foot Wind Tunnel
- Performance measurements of a pilot superconducting solenoid model core for a wind tunnel magnetic suspension and balance system
- Performance of the high speed anechoic wind tunnel at Lyon University
- Pioneer wind tunnels (with 4 plates)
- Porous wind tunnel corrections for counterrotation propeller testing
- Potential flow through a cascade of alternately displaced circular bodies : the rod-wall wind-tunnel boundary condition
- Practical aspects of laser holographic interferometry wind tunnels
- Prediction of vortex-induced loads on wind tunnel turning vanes
- Predictive wall adjustment strategy for two-dimensional flexible walled adaptive wind tunnel : a detailed description of the first one-step method
- Preliminary study of an apparatus to control the temperature of the flow entering the T2 cryogenic wind tunnel
- Problems associated with operations and measurement in cryogenic wind tunnels
- Procedure for computing transonic flows for control of adaptive wind tunnels
- Procedures and requirements for testing in the Langley Research Center Unitary Plan Wind Tunnel
- Progress in the Lewis Research Center altitude wind tunnel (AWT) modeling program
- Propulsion simulator for magnetically-suspended wind tunnel models
- Qualification of the T2 wind tunnel in cryogenic operation, A, Thermal field, preliminary study of a schematic model
- Qualification of the T2 wind tunnel in cryogenic operation, B, Particle detection and qualification
- Recent progress in the measurement of the drag coefficients of transport aircraft in a wind tunnel
- Remarks on the layout of the subsonic free jet wind tunnels
- Reports on wind tunnel experiments in aerodynamics : (with five plates)
- Research at NASA's NFAC wind tunnels
- Results of an icing test on a NACA 0012 airfoil in the NASA Lewis Icing Research Tunnel
- Results of design studies and wind tunnel tests of an advanced high lift system for an energy efficient transport
- Results of design studies and wind tunnel tests of high-aspect-ratio supercritical wings for an energy efficient transport
- Results of the AFRSI detailed-environment test of the 0.035-scale SSV pressure-loads model 84-0 in the Ames 11x11 ft. TWT and the Lewis 8x6 ft. and 10x10 ft. SWT (0A-310A, B, C)
- Reverberation effects on directionality and response of stationary monopole and dipole sources in a wind tunnel
- Review of aeronautical wind tunnel facilities
- Rotary balance data for an F-15 model with fuel tanks for an angle-of-attack range of 80
- Rotary balances : a selected, annotated bibliography
- STOL and STOVL hot gas ingestion and airframe heating tests in the NASA Lewis 9- by 15-foot low-speed wind tunnel
- Selected topics in experimental aeroelasticity at the NASA Langley Research Center
- Shake test results of the MDHC test stand in the 40- by 80-foot wind tunnel
- Some anomalies observed in wind-tunnel tests of a blunt body at transonic and supersonic speeds
- Some lessons learned with wind tunnels
- Space shuttle afterbody aerodynamics/plume simulation data summary
- Structural integrity of wind tunnel wooden fan blades
- Studies of condensation effects on airfoil testing in the Langley 0.3-meter transonic cryogenic tunnel
- Study of ice accretion on icing wind tunnel components
- Study of optical techniques for the Ames unitary wind tunnel, Part 4, Infrared imagery
- Study of optical techniques for the Ames unitary wind tunnels, Part 1, schlieren
- Study of optical techniques for the Ames unitary wind tunnels, Part 2, Light sheet and vapor screen
- Study of optical techniques for the Ames unitary wind tunnels, Part 3, Angle of attack
- Study of optical techniques for the Ames unitary wind tunnels, Part 4, Model deformation
- Study of optical techniques for the Ames unitary wind tunnels, Part 6, digital image processing
- Study of optical techniques for the Ames unitary wind tunnels, Part 7, final report
- Study on needs for a magnetic suspension system operating with a transonic wind tunnel
- Subsonic wind-tunnel measurements of a slender wing-body configuration employing a vortex flap
- Summary of life and lift/cruise fan powered lift concept technology
- Summary of low-speed wind tunnel results of several high-speed counterrotation propeller configurations
- Tests with three-dimensional adjustments in the rectangular working section of the French T2 wind tunnel, with an AS 07-type swept-back wing model
- The 13-inch magnetic suspension and balance system wind tunnel
- The Altitude wind tunnel (AWT)--a unique facility for propulsion system and adverse weather testing
- The F2 wind-tunnel at Fauga-Mauzac
- The Langley 14- by 22-foot subsonic tunnel : description, flow characteristics, and guide for users
- The NASA Altitude Wind Tunnel : its role in advanced icing research and development
- The NASA Lewis Research Center internal fluid mechanics facility
- The aerodynamic performance of several flow control devices for internal flow systems
- The design and operational development of self-streamlining two-dimensional flexible walled test sections
- The design and preliminary calibration of a boundary-layer flow channel
- The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel
- The influence of a wind tunnel on helicopter rotational noise : formulation of analysis
- Thermal/structural analysis of a transpiration cooled nozzle
- Time-averaged aerodynamic loads on the vane sets of the 40- by 80-foot and 80- by 120-foot wind tunnel complex
- Two dimensional aerodynamic interference effects on oscillating airfoils with flaps in ventilated subsonic wind tunnels
- Ultra-light duct for an anechoic wind tunnel
- Unsteady aerodynamic load estimates on turning vanes in the National Full-Scale Aerodynamic Complex
- Unsteady two dimensional airloads acting on oscillating thin airfoils in subsonic ventilated wind tunnels
- Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight
- User manual for 0.3-M TCT wall-interference assessment/correction procedure : 8- by 24-inch airfoil test section
- User's manual for the Langley Research Center 14- by 22-foot subsonic tunnel static data acquisition system
- User's manual for the model interface and plugboard cabinets in the 14- by 22-foot subsonic tunnel
- Wake characteristics of an eight-leg tower for a MOD-O type wind turbine
- Wind tunnel evaluation of particle sizing instruments
- Wind tunnel investigation of three axisymmetric cowls of different lengths at Mach numbers from 0.60 to 0.92
- Wind tunnel investigations of forebody strakes for yaw control on F/A-18 model at subsonic and transonic speeds
- Wind tunnel measurements of the tower shadow on models of the ERDA/NASA 100 kW wind turbine tower
- Wind tunnel requirements for computational fluid dynamics code verification
- Wind tunnel results of advanced high speed propellers in the takeoff, climb, and landing operating regimes
- Wind tunnel technology for the development of future commercial aircraft
- Wind tunnel test of 1/30 scale heliostat field array model : test report
- Wind tunnel test of a full-scale heliostat
- Wind tunnel test of a variable-diameter tiltrotor (VDTR) model
- Wind tunnel testing and research
- Wind tunnel tests of high-lift systems for advanced transports using high-aspect-ratio supercritical wings
- Wind tunnel tests of parabolic trough solar collectors, March 2001- August 2003
- Wind tunnel turning vanes of modern design
- Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps
- Wind-tunnel free-flight investigation of a model of a forward-swept-wing fighter configuration
- Wind-tunnel free-flight investigation of a supersonic persistence fighter
- Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow
- Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line
- Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
- Wind-tunnel investigation of an advanced general aviation canard configuration
- Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section
- Wind-tunnel study of wind loading on a compliant offshore platform
- Wind-tunnel/flight correlation, 1981 : proceedings of a miniworkshop held at NASA Langley Research Center, Hampton, Virginia, November 19-20, 1981
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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.library.in.gov/resource/v6Tx6rJVJ4c/" 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/v6Tx6rJVJ4c/">Wind tunnels</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>