Journals
Publish with us
Publishing partnerships
About us
Blog
International Journal of Aerospace Engineering
Journal overview
For authors
For reviewers
For editors
Table of Contents
Special Issues
International Journal of Aerospace Engineering
/
2017
/
Article
/
Fig 16
/
Research Article
Performance and Vibration Analyses of Lift-Offset Helicopters
Figure 16
Lift distributions at 140 knots in compound helicopter mode (LOS = 0.3).