Wind tunnels
Resource Information
The concept Wind tunnels represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
The Resource
Wind tunnels
Resource Information
The concept Wind tunnels represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
- Label
- Wind tunnels
- Authority link
- (EG-IN)676479
240 Items that share the Concept Wind tunnels
Context
Context of Wind tunnelsSubject of
No resources found
No enriched resources found
- 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 58ånd 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
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/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>
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 Wind tunnels
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/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>
