Institute of Aerodynamics and Gas Dynamics

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341 to 350 of 362 Results

naca_0.40-0.120_0.40-0.120.tar.bz2 Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor Bzip Archive - 1.6 GB - MD5: 7881b0fbefb57e3c3dbabae436634d50 CodeData OpenFOAM simulation results: symmetric NACA camber of 12% at position p = 0.4
naca_0.40-0.140_0.40-0.140.tar.bz2 Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor Bzip Archive - 1.7 GB - MD5: 1e9332915ecb5f5187efb00224fc026f CodeData OpenFOAM simulation results: symmetric NACA camber of 14% at position p = 0.4
naca_0.40-0.160_0.40-0.080.tar.bz2 Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor Bzip Archive - 1.7 GB - MD5: bb25341021cbf95fa7ddc714afc9544e CodeData OpenFOAM simulation results: asymmetric NACA camber with 16% camber at top and 8% camber at bottom, p=0.4
naca_0.40-0.160_0.40-0.160.tar.bz2 Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor Bzip Archive - 1.8 GB - MD5: 5019acd5fe7e23c4754eee81e69240e7 CodeData OpenFOAM simulation results: symmetric NACA camber of 16% at position p = 0.4
naca_0.50-0.120_0.50-0.120.tar.bz2 Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor Bzip Archive - 1.7 GB - MD5: 683108ed95f8ded14d99f761a4567e22 CodeData OpenFOAM simulation results: symmetric NACA camber of 12% at position p = 0.5
naca_0.60-0.120_0.60-0.120.tar.bz2 Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor Bzip Archive - 1.7 GB - MD5: 59eb75e1d98eb1fe5973b95d0d7d028c CodeData OpenFOAM simulation results: symmetric NACA camber of 12% at position p = 0.6
no_camber.tar.bz2 Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor Bzip Archive - 1.8 GB - MD5: 2d2b05e80873645832f5e0f77bf73999 CodeData OpenFOAM simulation results: baseline case with symmetric NACA0015 airfoils
pointDisplacement_scripts.tar Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor TAR Archive - 149.5 KB - MD5: bab852735d163da3e1e25e2ea7b2665d CodeData python scripts used for pointDisplacement file generation
Results_Summary.pdf Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor Adobe PDF - 223.7 KB - MD5: ef5840d3b88f6b994a5064779a0bc013 Documentation The thrust, power and efficiency results of all cases are concluded.
TE_0.20-0.100_0.20-0.100.tar.bz2 Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor Bzip Archive - 1.6 GB - MD5: b50d27ec01438d671be3bffa26f4c069 CodeData OpenFOAM simulation results: symmetric trailing edge camber of 10% at position p = 0.2

naca_0.40-0.120_0.40-0.120.tar.bz2

Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor

Bzip Archive - 1.6 GB -

CodeData

OpenFOAM simulation results: symmetric NACA camber of 12% at position p = 0.4

naca_0.40-0.140_0.40-0.140.tar.bz2

Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor

Bzip Archive - 1.7 GB -

CodeData

OpenFOAM simulation results: symmetric NACA camber of 14% at position p = 0.4

naca_0.40-0.160_0.40-0.080.tar.bz2

Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor

Bzip Archive - 1.7 GB -

CodeData

OpenFOAM simulation results: asymmetric NACA camber with 16% camber at top and 8% camber at bottom, p=0.4

naca_0.40-0.160_0.40-0.160.tar.bz2

Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor

Bzip Archive - 1.8 GB -

CodeData

OpenFOAM simulation results: symmetric NACA camber of 16% at position p = 0.4

naca_0.50-0.120_0.50-0.120.tar.bz2

Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor

Bzip Archive - 1.7 GB -

CodeData

OpenFOAM simulation results: symmetric NACA camber of 12% at position p = 0.5

naca_0.60-0.120_0.60-0.120.tar.bz2

Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor

Bzip Archive - 1.7 GB -

CodeData

OpenFOAM simulation results: symmetric NACA camber of 12% at position p = 0.6

no_camber.tar.bz2

Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor

Bzip Archive - 1.8 GB -

CodeData

OpenFOAM simulation results: baseline case with symmetric NACA0015 airfoils

pointDisplacement_scripts.tar

Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor

TAR Archive - 149.5 KB -

CodeData

python scripts used for pointDisplacement file generation

Results_Summary.pdf

Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor

Adobe PDF - 223.7 KB -

Documentation

The thrust, power and efficiency results of all cases are concluded.

TE_0.20-0.100_0.20-0.100.tar.bz2

Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor

Bzip Archive - 1.6 GB -

CodeData

OpenFOAM simulation results: symmetric trailing edge camber of 10% at position p = 0.2

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