Nonlinear aeroservoelastic analysis of a supersonic aircraft with control fin free-play by component mode synthesis technique
['Wei Tian', 'Yingsong Gu', 'Hao Liu', 'Xiaochen Wang', 'Ping Li']
/
Journal of Sound and Vibration
/ Vol. 493
0.0 / 5
0
Reviews
You must log in to post, edit and delete a review.
Log in
Earn 50 points when your review is published.
About KnowledgeRank Points
No reviews have been posted yet. Be the first to write one!