Aerodynamic Design of the NASA Rotor 67 for Non Uniform Inflow

PDF Publication Title:

Aerodynamic Design of the NASA Rotor 67 for Non Uniform Inflow ( aerodynamic-design-nasa-rotor-67-non-uniform-inflow )

Previous Page View | Next Page View | Return to Search List

Text from PDF Page: 010

Master Thesis Report List of Figures 5.431565BladeProfileleadingedgezoom............................ 57 5.441565BladeProfiletrailingedgezoom ........................... 57 5.45 Comparison of 2265 Mach Contour between 2D fitted and Actual Point Profile . . 5.46 Comparison of 2265 Pressure Contour between 2D fitted and Actual Point Profile 5.47 Comparison of 2265 Mach Contour between 2D fitted and Surface fitted Profile . . 5.48 Comparison of 2265 Pressure Contour between 2D fitted and Surface fitted Profile 5.49 Comparison of 2265 Mach Contour between Actual point and Surface fitted Profile 5.50 Comparison of 2265 Pressure Contour between Actual point and Surface fitted Profile 59 5.51 Comparison of 2265 Blade loading between 2D fitted and Actual point profile . . . 5.52 Comparison of 2265 Blade loading between 2D fitted and Surface Fitted profile . . 5.53 Comparison of 2265 Blade loading between Surface fitted and Actual point profile 5.54 Comparison of 2265 Blade Profiles from 3 Coordinate sources . . . . . . . . . . . . 5.552265BladeProfileleadingedgezoom.......................... 5.562265BladeProfiletrailingedgezoom ........................... 60 5.57Enthalpy-EntropydiagramofaStatorBlade ....................... 61 5.58AreaDistributionforvariousbladeprofiles ........................ 62 6.1 Featuresofagoodquality2Dmesh............................. 63 6.2 2DMeshGeneratedbySalome ............................... 64 6.3 LeadingedgezoomonSalome2DMesh .......................... 64 6.4 TrailingedgezoomonSalome2DMesh .......................... 64 6.5 BoundaryLayerzoomonSalome2DMesh ........................ 64 6.6 ComparisonofProfile1265SalomeandUMG2MeshMachContour . . . . . . . . . . 65 6.7 Comparison of Profile 1265 Salome and UMG 2 Mesh Pressure Contour . . . . . . . . 65 6.8 ComparisonofProfile1265SalomeandUMG2MeshBladeLoading . . . . . . . . . . 65 6.9 Featuresofagoodquality3Dmesh............................. 66 6.10 Fine Discretized Mesh across the Leading/Trailing edge and the Top/Bottom Blade Surfaces............................................ 66 6.11 ClippedVerticalViewofNASARotor67InternalMeshDomain . . . . . . . . . . . . 67 6.12 Clipped Horizontal View of NASA Rotor 67 Internal Mesh Domain . . . . . . . . . . . 67 6.133DmeshofCentrifugalRotorwithtipclearance ..................... 67 6.14 Clipped Vertical View of Centrifugal Rotor Internal Mesh Domain . . . . . . . . . . . 68 6.15 Clipped Cross-Section View of Centrifugal Rotor Internal Mesh Domain . . . . . . . . 68 6.16MachStreamlinesofWingProfile.............................. 68 6.17TopviewofMachcontourofWingDomain ........................ 68 6.18 PressureCoefficientPlotofSalomeMeshedWingSlice. . . . . . . . . . . . . . . . . . 69 6.19SU2MeshFormat ...................................... 70 7.1 SpanwiseTotalPressureatInlet/OutletBoundary . . . . . . . . . . . . . . . . . . . . 72 7.2 SpanwiseTotalTemperatureatInlet/OutletBoundary. . . . . . . . . . . . . . . . . . 72 7.3 SpanwiseStaticPressureatInlet/OutletBoundary . . . . . . . . . . . . . . . . . . . . 72 7.4 MeasurementPointsatInletandOutletBoundary .................... 72 7.5 Total Pressure Contour at the Inlet and Outlet Plane of the Inlet Configuration . . . . 73 7.6 Velocity Contour at the Inlet and Outlet Plane of the Inlet Configuration . . . . . . . 74 7.7 SampledPointsalongtheOutletPlaneofinletconfiguration . . . . . . . . . . . . . . 76 7.8 Plot of total pressure versus angular position for varying radial position . . . . . . . . 77 7.9 Plot of velocity versus angular position for varying radial position . . . . . . . . . . . . 77 7.10 Calculationofdistortionintensityatmidradius. . . . . . . . . . . . . . . . . . . . . . 78 7.11 Plot of Circumferential Averaged Total Pressure at various Spanwise Radial Position . 79 7.12IsometricViewof3DBladeAssembly ........................... 81 .. 58 .. 58 .. 58 .. 58 .. 59 .. 59 .. 59 .. 60 .. 60 .. 60 VIII

PDF Image | Aerodynamic Design of the NASA Rotor 67 for Non Uniform Inflow

PDF Search Title:

Aerodynamic Design of the NASA Rotor 67 for Non Uniform Inflow

Original File Name Searched:

nasa-rotor-67.pdf

DIY PDF Search: Google It | Yahoo | Bing

NFT (Non Fungible Token): Buy our tech, design, development or system NFT and become part of our tech NFT network... More Info

IT XR Project Redstone NFT Available for Sale: NFT for high tech turbine design with one part 3D printed counter-rotating energy turbine. Be part of the future with this NFT. Can be bought and sold but only one design NFT exists. Royalties go to the developer (Infinity) to keep enhancing design and applications... More Info

Infinity Turbine IT XR Project Redstone Design: NFT for sale... NFT for high tech turbine design with one part 3D printed counter-rotating energy turbine. Includes all rights to this turbine design, including license for Fluid Handling Block I and II for the turbine assembly and housing. The NFT includes the blueprints (cad/cam), revenue streams, and all future development of the IT XR Project Redstone... More Info

Infinity Turbine ROT Radial Outflow Turbine 24 Design and Worldwide Rights: NFT for sale... NFT for the ROT 24 energy turbine. Be part of the future with this NFT. This design can be bought and sold but only one design NFT exists. You may manufacture the unit, or get the revenues from its sale from Infinity Turbine. Royalties go to the developer (Infinity) to keep enhancing design and applications... More Info

Infinity Supercritical CO2 10 Liter Extractor Design and Worldwide Rights: The Infinity Supercritical 10L CO2 extractor is for botanical oil extraction, which is rich in terpenes and can produce shelf ready full spectrum oil. With over 5 years of development, this industry leader mature extractor machine has been sold since 2015 and is part of many profitable businesses. The process can also be used for electrowinning, e-waste recycling, and lithium battery recycling, gold mining electronic wastes, precious metals. CO2 can also be used in a reverse fuel cell with nafion to make a gas-to-liquids fuel, such as methanol, ethanol and butanol or ethylene. Supercritical CO2 has also been used for treating nafion to make it more effective catalyst. This NFT is for the purchase of worldwide rights which includes the design. More Info

NFT (Non Fungible Token): Buy our tech, design, development or system NFT and become part of our tech NFT network... More Info

Infinity Turbine Products: Special for this month, any plans are $10,000 for complete Cad/Cam blueprints. License is for one build. Try before you buy a production license. May pay by Bitcoin or other Crypto. Products Page... More Info

CONTACT TEL: 608-238-6001 Email: greg@infinityturbine.com (Standard Web Page)