Aeromechanical stability analysis of a hybrid heavy lift multirotor vehicle in hover
- 1 November 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 22 (11), 965-972
- https://doi.org/10.2514/3.45232
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Coupled helicopter rotor/body aeromechanical stability comparison oftheoretical and experimental resultsJournal of Aircraft, 1985
- Aeromechanical stability analysis of a multirotor vehicle model representing a hybrid heavy lift airship (HHLA)Published by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Heavy-lift airship dynamicsJournal of Aircraft, 1983