Flutter Analysis of Missile Control Surfaces Containing Structural Nonlinearities
- 1 October 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 18 (10) , 1245-1251
- https://doi.org/10.2514/3.50876
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- On limit cycling control systemsIEEE Transactions on Automatic Control, 1963
- An Approximate Analysis of Nonlinear Flutter ProblemsJournal of the Aerospace Sciences, 1959
- An Investigation of Effects of Certain Types of Structural NonHnearities on Wing and Control Surface FlutterJournal of the Aeronautical Sciences, 1957