Analytical treatment of wing divergence and flutter is in general very involved and often can be carried out only with simplifying assumptions; entirely different method of approach is to build elastically similar model and test it in wind tunnel; brief summary of similarity laws is presented.
Static and dynamic model similarity
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 6 , n 11 ; p 468-469
1939
2 pages
Bibliography
Article (Journal)
English
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