Transonic wind tunnels
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The concept Transonic wind tunnels represents the subject, aboutness, idea or notion of resources found in Missouri University of Science & Technology Library.
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Transonic wind tunnels
Resource Information
The concept Transonic wind tunnels represents the subject, aboutness, idea or notion of resources found in Missouri University of Science & Technology Library.
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- Transonic wind tunnels
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- nasat
47 Items that share the Concept Transonic wind tunnels
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- Two-dimensional wind tunnel
- 11 foot Unitary Plan tunnel facility optical improvement large window analysis
- A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel
- A historical overview of Aeroelasticity Branch and Transonic Dynamics Tunnel contributions to rotorcraft technology and development
- A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel
- Aerodynamic characteristics of two NASA supercritical airfoils with different maximum thicknesses
- 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
- Aeroservoelastic testing of free flying wind tunnel models
- An airfoil flutter model suspension system to accommodate large static transonic airloads
- Application of laser velocimetry to unsteady flows in large scale high speed tunnels
- Assessment of dual-point drag reduction for an executive-jet modified airfoil section
- Combustibility tests of 1,1,1,2-tetrafluoroethane in a simulated compressor cylinder
- Control of the NASA Langley 16-foot transonic tunnel with the self-organizing feature map
- Cryogenic pressure calibrator for wide temperature electronically scanned (ESP) pressure modules
- Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions
- Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions
- Demonstration of imaging flow diagnostics using Rayleigh scattering in Langley 0.3-Meter Transonic Cryogenic Tunnel
- Design study of advanced model support systems for the National Transonic Facility
- Development of a large field of view shadowgraph system for a 16 ft. transonic wind tunnel
- Evaluation of turbulence induced noise in coherent anti-stokes Raman scattering
- Experimental studies of transonic flow field near a longitudinally slotted wind tunnel wall
- Feasibility of Rayleigh scattering flow diagnostics in the National Transonic Facility
- Finite element analysis of a NASA National Transonic Facility wind tunnel balance
- Finite element analysis of a NASA National Transonic Facility wind tunnel balance
- Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport
- Langley 16-ft. Transonic Tunnel Pressure Sensitive Paint System
- Measuring global surface pressures on a circulation control concept using pressure sensitive paint
- Modeling and control study of the NASA 0.3-meter transonic cryogenic tunnel for use with sulfur hexafluoride medium
- Modifications to Langley 0.3-m TCT adaptive wall software for heavy gas test medium, Phase 1 studies
- Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment
- New coherent optical techniques for National Transonic Wind Tunnel Facility
- Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip
- Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip
- Pressure- and temperature-sensitive paint at 0.3-m transonic cryogenic tunnel
- R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
- Sidewall Mach number distributions for the NASA Langley Transonic Dynamics Tunnel
- Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊/
- Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf
- Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60°
- Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability
- Structural analysis of a thermal insulation retainer assembly
- The NASA Langley 16-foot transonic tunnel : historical overview, facility description, calibration, flow characteristics, and test capabilities
- The new heavy gas testing capability in the NASA Langley Transonic Dynamics Tunnel
- Transonic wind tunnel test of a 14% thick oblique wing
- Turbulence model comparisons for a high-speed aircraft
- Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoil
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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/qYLtLAr9ovY/" 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/qYLtLAr9ovY/">Transonic wind tunnels</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>
