%0 Report %1 1983nasa.reptS....L %A Lark, R. F. %A Gougeon, M. %A Thomas, G. %A Zuteck, M. %B National Aeronautics and Space Administration Report %D 1983 %E Pickett, J. S. %E Murphy, G. B. %E Kurth, W. S. %E Goertz, C. K. %E Shawhan, S. D. %K %T Fabrication of low-cost Mod-OA wood composite wind turbine blades %X The wood composite blades were fabricated by using epoxy resin-bonded laminates of Douglas fir veneers for the leading edge spar sections and honeycomb-cored birch plywood panels for the blade trailing edge or afterbody sections. The blade was joined to the wind turbine hub assembly by epoxy resin-bonded steel load take-off studs. The wood composite blades were installed in the Mod-OA wind turbine test facility at Kahuku, Hawaii. The wood composite blades have successfully completed high power (average of 150 kW) operations for an eighteen month period (nearly 8,000 hr) before replacement with another set of wood composite blades. The original set of blades was taken out of service because of the failure of the shank on one stud. An inspection of the blades at NASA-Lewis showed that the shank failure was caused by a high stress concentration at a corrosion pit on the shank fillet radius which resulted in fatigue stresses in excess of the endurance limit.

@techreport{1983nasa.reptS....L, abstract = {The wood composite blades were fabricated by using epoxy resin-bonded laminates of Douglas fir veneers for the leading edge spar sections and honeycomb-cored birch plywood panels for the blade trailing edge or afterbody sections. The blade was joined to the wind turbine hub assembly by epoxy resin-bonded steel load take-off studs. The wood composite blades were installed in the Mod-OA wind turbine test facility at Kahuku, Hawaii. The wood composite blades have successfully completed high power (average of 150 kW) operations for an eighteen month period (nearly 8,000 hr) before replacement with another set of wood composite blades. The original set of blades was taken out of service because of the failure of the shank on one stud. An inspection of the blades at NASA-Lewis showed that the shank failure was caused by a high stress concentration at a corrosion pit on the shank fillet radius which resulted in fatigue stresses in excess of the endurance limit.}, added-at = {2021-10-16T10:52:22.000+0200}, adsnote = {Provided by the SAO/NASA Astrophysics Data System}, adsurl = {http://adsabs.harvard.edu/abs/1983nasa.reptS....L}, author = {{Lark}, R. F. and {Gougeon}, M. and {Thomas}, G. and {Zuteck}, M.}, biburl = {https://www.bibsonomy.org/bibtex/22bd77831f5ead18f881ce7636e9328d5/woodsproductos}, booktitle = {National Aeronautics and Space Administration Report}, editor = {{Pickett}, J. S. and {Murphy}, G. B. and {Kurth}, W. S. and {Goertz}, C. K. and {Shawhan}, S. D.}, interhash = {3f3bf16f2155e605e6779d4b4a315f0f}, intrahash = {2bd77831f5ead18f881ce7636e9328d5}, keywords = {}, month = {February}, timestamp = {2021-10-16T10:52:22.000+0200}, title = {{Fabrication of low-cost Mod-OA wood composite wind turbine blades}}, year = 1983 }