Wind tunnel tests
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Wind tunnel tests
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- Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3
- 1-by 1- foot supersonic wind tunnel sidewall flowfield compression plate study
- 14- by 22-foot subsonic tunnel laser velocimeter upgrade
- 70 years of aeropropulsion research at NASA Glenn Research Center
- A basic robotic excavator (the "Glenn digger٣) : description, design, and initial operation
- A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet
- A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet
- A feasibility study to control airfoil shape using THUNDER
- A method for data base management and analysis for wind-tunnel data
- A study of large droplet ice accretion in the NASA Lewis IRT at near-freezing conditions; Pt. 2
- A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept
- A turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool
- A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel
- A wall interference assessment/correction interface measurement system for the NASA-ARC 12-FT PWT : final memorandum report
- A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
- A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
- A wind tunnel study of icing effects on a business jet airfoil
- A wind tunnel study on the Mars Pathfinder (MPF) lander descent pressure sensor
- A wind tunnel study on the Mars Pathfinder (MPF) lander descent pressure sensor
- Acoustic measurements from a rotor blade-vortex interaction noise experiment in the German-Dutch wind tunnel (DNW)
- Acoustic performance of drive rig mufflers for model scale engine testing
- Acoustic testing of a high-tip-speed fan with bypass-duct liners--overview
- Aero-heating of shallow cavities in hypersonic freestream flow
- Aero-thermal calibration of the NASA Glenn Icing Research Tunnel (2004 and 2005 tests)
- Aero-thermal calibration of the NASA Glenn Icing Research Tunnel (2012 tests)
- Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air
- Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air
- Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
- Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90
- Aerodynamic characteristics of two NASA supercritical airfoils with different maximum thicknesses
- Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations
- Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel
- Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel
- Aerodynamic parameters of an advanced fighter aircraft estimated from flight data : preliminary results
- Aerodynamic performance of a 0.27-scale model of an AH-64 helicopter with baseline and alternate rotor blade sets
- Aerodynamic simulation of ice accretion on airfoils
- Aeroservoelastic testing of free flying wind tunnel models
- Aerothermal analysis of a wing-elevon cove with variable leakage
- Aerothermal environment in chordwise gaps between split elevons at Mach 6.8
- Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions
- Aerothermodynamic measurement and prediction for modified orbiter at Mach 6 and 10
- Airloads on bluff bodies, with application to the rotor-induced downloads on tilt-rotor aircraft
- An aeroelastician's perspective of wind tunnel and flight experiences with active control of structural response and stability
- An assessment of 3-C PIV analysis methodology for HART II measured data
- An evaluation of measured pressure signatures from wind-tunnel models of three low-boom concepts
- An experimental and numerical study of icing effects on the performance and controllability of a twin engine aircraft
- An experimental approach to a rapid propulsion and aeronautics concepts testbed
- An experimental investigation of the ground vortex created by a moving jet
- An experimental investigation on location of boundary layer transition on the NACA 0012 using surface hot film gages
- An interactive software for conceptual wing flutter analysis and parametric study
- An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner
- An investigation of the causes of failure of flexible thermal protection materials in an aerodynamic environment
- An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5
- Analysis and test evaluation of the dynamic stability of three advanced turboprop models at zero forward speed
- Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation
- Analysis of wind tunnel longitudinal static and oscillatory data of the F-16XL aircraft
- Analysis of wind tunnel longitudinal static and oscillatory data of the F-16XL aircraft
- Application of rapid prototyping methods to high-speed wind tunnel testing (MSFC Center Director's Discretionary Fund final report, project no. 96-21)
- Application of wind tunnel free-flight technique for wake vortex encounters
- Assessment of NASA's aircraft noise prediction capability
- Benefits of swept and leaned stators for fan noise reduction
- Benefits of swept and leaned stators for fan noise reduction
- Body-freedom flutter of a 1/2 scale forward-swept-wing-model, an experimental and analytical study
- Boeing SMART rotor full-scale wind tunnel test data report
- Boundary layer transition in the leading edge region of a swept cylinder in high speed flow
- CFD analysis of nozzle jet plume effects on sonic boom signature
- CFD study of NACA 0018 airfoil with flow control
- Calibration of the NASA Glenn 8- by 6-foot supersonic wind tunnel (1996 and 1997 tests)
- Cavity heating experiments supporting Shuttle Columbia accident investigation
- Comparison of DAC and MONACO DSMC codes with flat plate simulation
- Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack
- Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack
- Comprehensive report of fan performance from duct rake instrumentation on 1.294 pressure ratio, 806 ft/sec tip speed turbofan simulator models
- Computational aerodynamic simulations of a 1484 ft/sec tip speed quiet high-speed fan system model for acoustic methods assessment and development
- Computational analysis of a low-boom supersonic inlet
- Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition
- Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations
- Computational test cases for a rectangular supercritical wing undergoing pitching oscillations
- Cruise noise of the SR-2 propeller model in a wind tunnel
- Cryogenic pressure calibrator for wide temperature electronically scanned (ESP) pressure modules
- Description of the U.S. Army small-scale 2-meter rotor test system
- Design and fabrication of the NASA decoupler pylon for the F-16 aircraft
- Design of the wind tunnel model communication controller board
- Design study of an entry probe spectro-reflectometer
- Determination of HART I blade structural properties by laboratory testing
- Determination of turbine blade life from engine field data
- Development and characterization testing of an air pulsation valve for a pulse detonation engine supersonic parametric inlet test section
- Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8
- Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8
- Development of experimental icing simulation capability for full-scale swept wings : hybrid design process, years 1 and 2
- Development of microchannel plates in advanced wind-tunnel instrumentation
- Digital-flutter-suppression-system investigations for the active flexible wing wind-tunnel model
- Dynamic response of a hammerhead launch vehicle wind-tunnel model
- Dynamic wind-tunnel testing of a sub-scale iced S-3B Viking
- Effect of fin leading edge sweep on shock-shock interaction at Mach 6
- Effect of in-flight ice accretion on the performance of a multi-element airfoil
- Effectiveness of micro-blowing technique in adverse pressure gradients
- Effectiveness of micro-blowing technique in adverse pressure gradients
- Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle
- Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles
- Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration
- Engineering aerothermal analysis for X-34 thermal protection system design : 36th Aerospace Sciences meeting & exhibit : January 12-15, 1998/Reno, NV
- Estimated benefits of variable-geometry wing camber control for transport aircraft
- Estimated benefits of variable-geometry wing camber control for transport aircraft
- Estimates for the aerodynamic coefficients of ringsail and disk-gap-band parachutes operating on Mars
- Estimation of aircraft nonlinear unsteady parameters from wind tunnel data
- Estimation of aircraft nonlinear unsteady parameters from wind tunnel data
- Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight
- Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight
- Evaluation of gritting strategies for high angle of attack using wind tunnel and flight test data for the F/A-18
- Evaluation of the feasibility of scale modeling to quantify wind and terrain effects on low-angle sound propagation
- Experimental aerodynamic heating to simulated shuttle tiles
- Experimental aeroelasticity history, status and future in brief
- Experimental aerothermodynamic research of hypersonic aircraft : final technical report, for the period March 1, 1986 - July 31, 1990
- Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly
- 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 parametric study of jet vortex generators for flow separation control
- Experimental sonic boom measurements on a Mach 1.6 cruise low-boom configuration
- Experimental studies of transonic flow field near a longitudinally slotted wind tunnel wall
- Experimental study of boundary layer behavior in a simulated low pressure turbine
- Experimental study of convective heating on the back face and payload of a Hypersonic Inflatable Aerodynamic Decelerator (HIAD) aeroshell
- Experimental surface pressure data obtained on 65 ° delta wing across Reynolds number and Mach number ranges
- Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges
- Exploratory investigation of forebody strakes for yaw control of a generic fighter with a symmetric 600 half-angle chine forebody
- Exploratory low-speed wind-tunnel study of concepts designed to improve aircraft stability and control at high angles of attack
- Exploratory studies in generalized predictive control for active gust load alleviation
- Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack
- F-18 High Alpha Research Vehicle surface pressures : initial in-flight results and correlation with flow visualization and wind-tunnel data
- F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack : contract NAS 3-26617
- Factors influencing pitot probe centerline displacement in a turbulent supersonic boundary layer
- Factors influencing pitot probe centerline displacement in a turbulent supersonic boundary layer
- Flight services and aircraft access : active flow control vertical tail and insect accretion and mitigation flight test
- Flight stability and control and performance results from the Linear Aerospike SR-71 Experiment (LASRE)
- Flight test identification and simulation of a UH-60A helicopter and slung load
- Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds
- Flow control under low-pressure turbine conditions using pulsed jets : final report
- Flow quality studies of the NASA Glenn Research Center Icing Research Tunnel circuit (1995 tests
- Flow quality studies of the NASA Glenn Research Center Icing Research Tunnel circuit (1995 tests)
- Flow quality survey of the 8-by 6-foot supersonic wind tunnel (2015 test) prior to the 9-by 15-foot low-speed wind tunnel acoustic improvement modifications
- Flow quality surveys in the settling chamber of the NASA Glenn icing research tunnel (2011 tests)
- Flow unsteadiness effects on boundary layers
- Flow-visualization techniques used at high speed by configuration aerodynamics wind-tunnel-test team
- Fluorescence-doped particles for simultaneous temperature and velocity imaging
- Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil
- Fundamental ice crystal accretion physics studies
- Further assessment of MVD effects in SLD applications
- High accuracy temperature measurements using RTD's with current loop conditioning
- High-temperature modal survey of a hot-structure control surface
- Hot-bench simulation of the active flexible wing wind-tunnel model
- Hybrid wing body shielding studies using an ultrasonic configurable fan artificial noise source generating typical turbofan modes
- Hypersonic boundary-layer transition for X-33 phase II vehicle
- Icing Research Tunnel (IRT) Force Measurement System (FMS)
- Improvements to the total temperature calibration of the NASA Glenn Icing Research Tunnel
- In-flight aerodynamic measurements of an iced horizontal tailplane
- Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance
- Initial investigation of the acoustics of a counter-rotating open rotor model with historical baseline blades in a low-speed wind tunnel
- Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector
- Investigation of solid plume simulation criteria to produce flight plume effects on multibody configuration in wind tunnel tests
- Investigation of solid plume simulation criteria to produce flight plume effects on multibody configuration in wind tunnel tests
- Investigation of unsteady pressure-sensitive paint (uPSP) and a dynamic loads balance to predict launch vehicle buffet environments
- Isokinetic TWC evaporator probe : calculations and systemic uncertainty analysis
- Isokinetic TWC evaporator probe : development of the IKP2 and performance testing for the HAIC-HIWC Darwin 2014 and Cayenne-2015 field campaigns
- Lateral jet injection into typical combustor flowfields
- Lewis Icing Research Tunnel test of the aerodynamic effects of aircraft ground deicing/anti-icing fluids
- Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivatives for the X-29A aircraft
- Low-speed wind tunnel tests of two waverider configuration models
- Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊/
- Low-speed wind-tunnel results for symmetrical NASA LS(1)-0013 airfoil
- Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
- Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode
- MAVRIC flutter model transonic limit cycle oscillation test
- MAVRIC flutter model transonic limit cycle oscillation test
- Mach 10 experimental database of a three-dimensional scramjet inlet flow field
- Mach 5 inlet CFD and experimental results
- Mach 6 flow field surveys beneath the forebody of an airbreathing missile
- Mars tumbleweed : FY2003 conceptual design assessment
- Measured sonic boom signatures above and below the XB-70 airplane flying at Mach 1.5 and 37,000 feet
- Measurements of a single lateral jet injected into swirling crossflow
- Mid-fidelity computational fluid dynamics analysis of the Elytron 4S UAV concept
- Modeling of longitudinal unsteady aerodynamics of a wing-tail combination
- Modifications to the 4 x 7 meter tunnel for acoustic research : engineering feasibility study
- NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6
- NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6
- Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds
- Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle
- Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle
- Navier-Stokes simulation of several high-lift reference H configurations
- Neural network prediction of new aircraft design coefficients
- Noise of a simulated installed model counter rotation propeller at angle-of-attack and takeoff/approach conditions
- Numerical solutions of the Navier-Stokes equations for transonic afterbody flows
- On hammershock propagation in a supersonic flow field
- Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel
- Orion Multi-Purpose Crew Vehicle (MPCV) Capsule Parachute Assembly System (CPAS) wake deficit wind tunnel testing
- Overview of HATP experimental aerodynamics data for the baseline F/A-18 configuration : High-Angle-of-Attack Technology Conference
- Parametric data from a wind tunnel test on a rocket-based combined-cycle engine inlet
- Parametric data from a wind tunnel test on a rocket-based combined-cycle engine inlet
- Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20
- Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip
- Performance data from a wind-tunnel test of two main-rotor blade designs for a utility-class helicopter
- Performance optimization of a rotor alone Nacelle for acoustic fan testing
- Performance optimization of a rotor alone Nacelle for acoustic fan testing
- Performance tests for the NASA Ames Research Center 20 cm x 40 cm oscillating flow wind tunnel : progress report
- Porous and microporous honeycomb composites as potential boundary-layer bleed materials
- Potential benefits of magnetic suspension and balance systems
- Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
- Pressure probe designs for dynamic pressure measurements in a supersonic flow field
- Quantitative global heat transfer in a Mach-6 quiet tunnel
- Reducing wind tunnel data requirements using neural networks
- Research and applications in aeroelasticity and structural dynamics at the NASA Langley Research Center
- Results of A M : 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42)
- Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A & C (IH-97A/B/C
- Results of aerothermodynamic and boundary layer transition testing of 0.0362-Scale X-38 (Rev 3.1) vehicle in NASA Langley 20-inch Mach 6 tunnel
- Results of an experimental program investigating the effects of simulated ice on the performance of the NACA 63A415 airfoil with flap
- Results of design studies and wind tunnel tests of an advanced high lift system for an energy efficient transport
- Results of the AFRSI rewaterproofing systems screening test in the NASA/AMES Research Center (ARC) 2x2-foot transonic wind tunnel (OS-310
- Review of blunt body wake flows at hypersonic low density conditions
- Review of blunt body wake flows at hypersonic low density conditions
- Review of the Aerodynamic Acceptance Test and application to anti-icing fluids testing in the NRC propulsion and icing wind tunnel
- Role of computational fluid dynamics and wind tunnels in aeronautics R&D
- Rotor CFD analysis at terrestrial and martian atmospheric densities
- Scaling of lift degradation due to anti-icing fluids based upon the aerodynamic acceptance test
- Shock generation and control using DBD plasma actuators : SBIR phase I final report
- Simultaneous optical measurements of axial and tangential steady-state blade deflections
- Space shuttle afterbody aerodynamics/plume simulation data summary
- Space shuttle orbiter trimmed center-of-gravity extension study : summary report
- Space shuttle orbiter trimmed center-of-gravity extension study, Volume ix, Effects of configuration modifications on the aerodynamic characteristics of the 140 A/B orbiter at mach numbers of 1.5, 2.0, and 2.5
- Space shuttle phase B wind tunnel model and test information, Volume 1, Booster configuration
- Space shuttle phase B wind tunnel model and test information, Volume 2, Orbiter configuration
- Space shuttle phase B wind tunnel model and test information, Volume 3, Launch configuration
- Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability
- Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities
- Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap
- Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊/
- Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles
- Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform
- Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations
- Study of several factors affecting crew escape trajectories from the space shuttle orbiter at low-subsonic speeds
- Study of the integration of wind tunnel and computational methods for aerodynamic configurations
- Subsonic aerodynamic characteristics of a circular body Earth-to-orbit vehicle
- Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle
- Subsonic and transonic pressure measurements on a high-aspect-ratio supercritical-wing model with oscillating control surfaces
- Subsonic dynamics of stardust sample return capsule
- Subsonic investigation of a leading-edge boundary layer cont[r]ol suction system on a high-speed civil transport configuration
- Subsonic investigation of a leading-edge boundary layer control suction system on a high-speed civil transport configuration
- Summary of the 2017 blockage test in the 10- by 10-foot supersonic wind tunnel
- Supersonic retropropulsion test 1853 in NASA LaRC Unitary Plan Wind Tunnel test section 2
- Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system
- Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system
- System dynamic analysis of a wind tunnel model with applications to improve aerodynamic data quality : a dissertation ...
- Tabulation of data from tests of an NPL 9510 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
- Takeoff/approach noise for a model counterrotation propeller with a forward-swept upstream rotor
- The F/A-18 high-angle-of-attack ground-to-flight correlation : lessons learned
- The beginner's guide to wind tunnels with TunnelSim and TunnelSys
- The effect of vortex generators on a jet in a cross-flow
- The history of the XV-15 tilt rotor research aircraft : from concept to flight
- Three-dimensional flow field measurements in a transonic turbine
- Three-dimensional flow field measurements in a transonic turbine cascade
- Transonic wind tunnel test of a 14% thick oblique wing
- Turbulence measurements in the near field of a wingtip vortex
- Turbulence measurements in the near field of a wingtip vortex
- Turbulence model comparisons for a high-speed aircraft
- Turbulent Navier-Stokes flow analysis of an advanced semispan diamond-wing model in tunnel and free air at high-lift conditions
- Two-dimensional wind tunnel
- UAS integration in the NAS project : flight test 3 data analysis of JADEM-autoresolver detect and avoid system
- Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight
- Unstructured grid Euler method assessment for longitudinal and lateral/directional aerodynamic performance analysis of the HSR technology concept airplane at supersonic cruise speeds
- Using pressure sensitive paint to measure aerodynamic forces on a rotor blade in hover
- V/STOL wind-tunnel testing
- Validation of 3-D ice accretion measurement methodology for experimental aerodynamic simulation
- Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel
- Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section
- Wind erosion in semiarid landscapes : predictive models and remote sensing methods for the influence of vegetation : semiannual status report for July 1, 1992 to December 31, 1992
- Wind tunnel acoustic study of a propeller installed behind an airplane empennage : data report
- Wind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles
- Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing
- Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing
- Wind tunnel simulations of aeolian processes
- Wind tunnel tests of rotor blade sections with replications of ice formations accreted in hover
- Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes
- Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter
- Wind-tunnel evaluation of the effect of blade nonstructural mass distribution on helicopter fixed-system loads
- Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4
- Wind-tunnel investigation of a full-scale canard-configured general aviation airplane
- Wind-tunnel investigation of a full-scale canard-configured general aviation airplane
- Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow
- Wind-tunnel investigations of blunt-body drag reduction using forebody surface roughness
- Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness
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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.mst.edu/resource/vUxM3uTOTvk/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.mst.edu/resource/vUxM3uTOTvk/">Wind tunnel tests</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.mst.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.mst.edu/">Missouri University of Science & Technology Library</a></span></span></span></span></div>
