@article{(Open Science Index):https://publications.waset.org/pdf/10007107,
	  title     = {Numerical and Experimental Investigations of Cantilever Rectangular Plate Structure on Subsonic Flutter},
	  author    = {Mevlüt Burak Dalmış and  Kemal Yaman},
	  country	= {},
	  institution	= {},
	  abstract     = {In this study, flutter characteristics of cantilever rectangular plate structure under incompressible flow regime are investigated by comparing the results of commercial flutter analysis program ZAERO© with wind tunnel tests conducted in Ankara Wind Tunnel (ART). A rectangular polycarbonate (PC) plate, 5x125x1000 mm in dimensions, is used for both numerical and experimental investigations. Analysis and test results are very compatible with each other. A comparison between two different solution methods (g and k-method) of ZAERO© is also done. It is seen that, k-method gives closer result than the other one. However, g-method results are on conservative side and it is better to use conservative results namely g-method results. Even if the modal analysis results are used for the flutter analysis for this simple structure, a modal test should be conducted in order to validate the modal analysis results to have accurate flutter analysis results for more complicated structures.
},
	    journal   = {International Journal of Aerospace and Mechanical Engineering},
	  volume    = {9},
	  number    = {11},
	  year      = {2015},
	  pages     = {2031 - 2038},
	  ee        = {https://publications.waset.org/pdf/10007107},
	  url   	= {https://publications.waset.org/vol/107},
	  bibsource = {https://publications.waset.org/},
	  issn  	= {eISSN: 1307-6892},
	  publisher = {World Academy of Science, Engineering and Technology},
	  index 	= {Open Science Index 107, 2015},
	}