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Structural qualification testing and operational loading on a fiberglass rotor blade for the Mod-OA wind turbineFatigue tests were performed on full- and half-scale root end sections, first to qualify the root retention design, and second to induce failure. Test methodology and results are presented. Two operational blades were proof tested to design limit load to ascertain buckling resistance. Measurements of natural frequency, damping ratio, and deflection under load made on the operational blades are documented. The tests showed that all structural design requirements were met or exceeded. Blade loads measured during 3000 hr of field operation were close to those expected. The measured loads validated the loads used in the fatigue tests and gave high confidence in the ability of the blades to achieve design life.
Document ID
19830015439
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Sullivan, T. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1983
Subject Category
Energy Production And Conversion
Report/Patent Number
E-1548
NASA/DOE/20320-44
NASA-TM-83309
NAS 1.15:83309
Report Number: E-1548
Report Number: NASA/DOE/20320-44
Report Number: NASA-TM-83309
Report Number: NAS 1.15:83309
Accession Number
83N23710
Funding Number(s)
PROJECT: RTOP 776-33-41
CONTRACT_GRANT: DE-AI01-76ET-20320
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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