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Methodology Of Blade Unsteady Pressure Measurement In The Nasa Transonic Flutter Cascade
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Author :National Aeronautics and Space Adm Nasa Publisher :Independently Published ISBN 13 :9781723859526 Total Pages :56 pages Book Rating :4.8/5 (595 download)
Book Synopsis Methodology of Blade Unsteady Pressure Measurement in the NASA Transonic Flutter Cascade by : National Aeronautics and Space Adm Nasa
Download or read book Methodology of Blade Unsteady Pressure Measurement in the NASA Transonic Flutter Cascade written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-09-20 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: In this report the methodology adopted to measure unsteady pressures on blade surfaces in the NASA Transonic Flutter Cascade under conditions of simulated blade flutter is described. The previous work done in this cascade reported that the oscillating cascade produced waves, which for some interblade phase angles reflected off the wind tunnel walls back into the cascade, interfered with the cascade unsteady aerodynamics, and contaminated the acquired data. To alleviate the problems with data contamination due to the back wall interference, a method of influence coefficients was selected for the future unsteady work in this cascade. In this approach only one blade in the cascade is oscillated at a time. The majority of the report is concerned with the experimental technique used and the experimental data generated in the facility. The report presents a list of all test conditions for the small amplitude of blade oscillations, and shows examples of some of the results achieved. The report does not discuss data analysis procedures like ensemble averaging, frequency analysis, and unsteady blade loading diagrams reconstructed using the influence coefficient method. Finally, the report presents the lessons learned from this phase of the experimental effort, and suggests the improvements and directions of the experimental work for tests to be carried out for large oscillation amplitudes.Lepicovsky, J. and McFarland, E. R. and Capece, V. R. and Jett, T. A. and Senyitko, R. G.Glenn Research CenterTRANSONIC FLUTTER; UNSTEADY AERODYNAMICS; ROTARY WINGS; COMPUTERIZED SIMULATION; WIND TUNNELS; PRESSURE MEASUREMENT; DATA INTEGRATION; DATA PROCESSING; NUMERICAL ANALYSIS; PHASE SHIFT; INFLUENCE COEFFICIENT; WIND TUNNEL WALLS
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