Institute of Aerodynamics and Gas Dynamics

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341 to 350 of 374 Results

LE_0.30-0.060_0.30-0.020.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: 3b180df38b6e10c9bdc5ac8d806cd26a CodeData OpenFOAM simulation results: asymmetric leading edge camber: 6% camber at top and 2% camber at bottom, p=0.3
LE_0.30-0.060_0.30-0.060.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: 44b2e1dfc7d4249c20895de03d05fceb CodeData OpenFOAM simulation results: symmetric leading edge camber of 6% at position p = 0.3
LE_0.30-0.080_0.30-0.080.tar.bz2 Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor Bzip Archive - 1.8 GB - MD5: 55ec0e48e7dda5a02e5c08586fa363ce CodeData OpenFOAM simulation results: symmetric leading edge camber of 8% at position p = 0.3
LE_0.30-0.120_0.30-0.120.tar.bz2 Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor Bzip Archive - 1.8 GB - MD5: a747d5f126d3d40123c6d4668cf43725 CodeData OpenFOAM simulation results: symmetric leading edge camber of 12% at position p = 0.3
LE_0.50-0.040_0.50-0.040.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: 5841eefc30f627574c9857cc10326b25 CodeData OpenFOAM simulation results: symmetric leading edge camber of 4% at position p = 0.5
Mesh description.7z Oct 21, 2021 - Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor 7Z Archive - 6.2 MB - MD5: 2576195d1d52693f9c9627fcac91d9d8 Pointwise file and exported polyMesh for OpenFOAM
naca_0.20-0.120_0.20-0.120.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: 35a21f1f92ac080a49447c54bfccc7b7 CodeData OpenFOAM simulation results: symmetric NACA camber of 12% at position p = 0.2
naca_0.30-0.120_0.30-0.120.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: b7535039fafbf435e88b1f609e3fca22 CodeData OpenFOAM simulation results: symmetric NACA camber of 12% at position p = 0.3
naca_0.40-0.040_0.40-0.040.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: 382b4f67da342c592a7011c19bf387cc CodeData OpenFOAM simulation results: symmetric NACA camber of 4% at position p = 0.4
naca_0.40-0.080_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 - 1.8 GB - MD5: 7fe4f3b4f7a4df41823463967021e743 CodeData OpenFOAM simulation results: symmetric NACA camber of 8% at position p = 0.4

LE_0.30-0.060_0.30-0.020.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: asymmetric leading edge camber: 6% camber at top and 2% camber at bottom, p=0.3

LE_0.30-0.060_0.30-0.060.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 leading edge camber of 6% at position p = 0.3

LE_0.30-0.080_0.30-0.080.tar.bz2

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

Bzip Archive - 1.8 GB -

CodeData

OpenFOAM simulation results: symmetric leading edge camber of 8% at position p = 0.3

LE_0.30-0.120_0.30-0.120.tar.bz2

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

Bzip Archive - 1.8 GB -

CodeData

OpenFOAM simulation results: symmetric leading edge camber of 12% at position p = 0.3

LE_0.50-0.040_0.50-0.040.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 leading edge camber of 4% at position p = 0.5

Mesh description.7z

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

7Z Archive - 6.2 MB -

Pointwise file and exported polyMesh for OpenFOAM

naca_0.20-0.120_0.20-0.120.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 = 0.2

naca_0.30-0.120_0.30-0.120.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 = 0.3

naca_0.40-0.040_0.40-0.040.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 4% at position p = 0.4

naca_0.40-0.080_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 - 1.8 GB -

CodeData

OpenFOAM simulation results: symmetric NACA camber of 8% at position p = 0.4

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