Nonlinear aeroelasticity Export

@article{Dowell2003, abstract = {Substantial progress has been made in modeling and understanding nonlinear aeroelastic phenomena. Experimental and theoretical investigations have shown good correlation for a number of nonlinear physical mechanisms. A number of physical mechanisms can lead to nonlinear aeroelastic response including the impact of static fluid or static structural nonlinearities in changing the flutter boundary of an aeroelastic system. The good news is that finite amplitude oscillations can in some cases replace what would otherwise be the rapidly growing and destructive oscillations of classical flutter behavior.}, address = {Texas A and M University, College Station, TX 77843-3141, United States}, author = {Dowell, E. and Edwards, J. and Strganac, T.}, citeulike-article-id = {2908038}, citeulike-linkout-0 = {http://www.scopus.com/record/display.url?view=extended&origin=resultslist&eid=2-s2.0-0242336478}, citeulike-linkout-1 = {http://www.scopus.com/scopus/record/display.url?view=extended&origin=resultslist&eid=2-s2.0-0242336478}, journal = {Journal of Aircraft}, keywords = {aeroelasticity, cosdyna, lco, review}, number = {5}, pages = {857--874}, posted-at = {2008-06-19 17:22:26}, priority = {2}, title = {Nonlinear aeroelasticity}, url = {http://www.scopus.com/scopus/record/display.url?view=extended&origin=resultslist&eid=2-s2.0-0242336478}, volume = {40}, year = {2003} }

TY - JOUR ID - Dowell2003 L3 - citeulike-article-id:2908038 N2 - Substantial progress has been made in modeling and understanding nonlinear aeroelastic phenomena. Experimental and theoretical investigations have shown good correlation for a number of nonlinear physical mechanisms. A number of physical mechanisms can lead to nonlinear aeroelastic response including the impact of static fluid or static structural nonlinearities in changing the flutter boundary of an aeroelastic system. The good news is that finite amplitude oscillations can in some cases replace what would otherwise be the rapidly growing and destructive oscillations of classical flutter behavior. IS - 5 JF - Journal of Aircraft AD - Texas A and M University, College Station, TX 77843-3141, United States EP - 874 TI - Nonlinear aeroelasticity VL - 40 SP - 857 KW - aeroelasticity KW - cosdyna KW - lco KW - review AU - Dowell, E AU - Edwards, J AU - Strganac, T PY - 2003/// UR - http://www.scopus.com/record/display.url?view=extended&origin=resultslist&eid=2-s2.0-0242336478 ER -