Method for the solution of the aeroelastic response problem for rotating wings
- 30 November 1966
- journal article
- Published by Elsevier in Journal of Sound and Vibration
- Vol. 4 (3) , 445-489
- https://doi.org/10.1016/0022-460x(66)90139-8
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- A METHOD FOR COMPUTING ROTARY WING AIRLOAD DISTRIBUTION IN FORWARD FLIGHTPublished by Defense Technical Information Center (DTIC) ,1962
- Airfoil Theory for Non-Uniform MotionJournal of the Aeronautical Sciences, 1938