Optimum Design of a Compound Helicopter
- 1 July 2009
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 46 (4) , 1210-1221
- https://doi.org/10.2514/1.40101
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Prediction of Rotor Structural Loads with Comprehensive AnalysisJournal of the American Helicopter Society, 2008
- Aeromechanics Analysis of a Heavy Lift Slowed-Rotor Compound HelicopterJournal of Aircraft, 2007
- Assessment of Comprehensive Analysis Calculation of Airloads on Helicopter RotorsJournal of Aircraft, 2005
- Performance Analysis of a Utility Helicopter with Standard and Advanced RotorsJournal of the American Helicopter Society, 2004