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  • 1
    Publication Date: 2019-06-27
    Description: Wind tunnel experiments were conducted on four small-scale flow-direction vanes for the determination of aerodynamic response. The tests were further extended to include a standard sized low-inertia vane currently employed in aircraft flight testing. The four test vanes had different aspect ratios and were about 35 percent of the surface area of the standard vane. The test results indicate satisfactory damping and frequency response for all vanes tested and compare favorably with the standard design.
    Keywords: AERODYNAMICS
    Type: NASA-CR-132545
    Format: application/pdf
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  • 2
    facet.materialart.
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    In:  Other Sources
    Publication Date: 2019-07-13
    Description: Experiments were performed to determine the torque required for rotating a rotor disk fitted with a number of radially arranged rods placed into a ducted airflow. An array of stationary rods, also radially arranged, was placed upstream close to the rotor with a small gap between the rods to cause wake interference. The results show that torque generally increased with airflow and the rate of increase varied considerably. At lower values of airflow, the rate of increase was larger than at higher airflow, and definite torque peaks occurred at certain airflow rates, where the torque attained a maximum within the test airflow range. During the test, a maximum blade passage frequency of 2037 Hz was attained. The results also show that the torque peaks occurred at the same Strouhal number for all speeds.
    Keywords: AERODYNAMICS
    Type: ASME PAPER 79-WA/FE-23 , Winter Annual Meeting; Dec 02, 1979 - Dec 07, 1979; New York, NY
    Format: text
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  • 3
    Publication Date: 2019-06-27
    Description: Experiments were performed to determine the power required for rotating a rotor disc fitted with a number of radially arranged rods placed into a ducted airflow. An array of stationary rods, also radially arranged, were placed upstream close to the rotor with a small gap between the rods to cause wake interference. The results show that power increased with increasing airflow and the rate of increase varied considerably. At lower values of airflow the rate of increase was larger than at higher airflow and definite power peaks occurred at certain airflow rates, where the power attained a maximum within the test airflow range. During the test a maximum blade passage frequency of 2037 Hz was attained.
    Keywords: AERODYNAMICS
    Type: NASA-CR-132556 , TR-74-M6
    Format: application/pdf
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