Computational Fluid Dynamics—Computational Structural Dynamics Analysis of Active Control of Helicopter Rotor for Performance Improvement
Authors:
- Rohit JainRJRohit Jain
- Hyeonsoo YeoHYHyeonsoo Yeo
- Inderjit ChopraICInderjit Chopra
- 1 January 2010
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 55 (4)
Abstract
No abstract availableThis publication has 20 references indexed in Scilit:
- Dynamic Blade Shape for Improved Helicopter Rotor PerformanceJournal of the American Helicopter Society, 2010
- Coupled CFD/CSD Prediction of the Effects of Trailing Edge Flaps on Rotorcraft Dynamic Stall Alleviation2009
- Assessment of Active Controls for Rotor Performance EnhancementJournal of the American Helicopter Society, 2008
- Rotor Airloads Prediction Using Loose Aerodynamic/Structural CouplingJournal of Aircraft, 2006
- Optimum Two-Per-Revolution Inputs for Improved Rotor PerformanceJournal of Aircraft, 2005
- Adaptive Airfoil Dynamic Stall Control2005
- Smart Material-Actuated Rotor Technology – SMARTJournal of Intelligent Material Systems and Structures, 2004
- Review of State of Art of Smart Structures and Integrated SystemsAIAA Journal, 2002
- Modeling rotorcraft dynamics with finite element multibody proceduresMathematical and Computer Modelling, 2001
- Status of Application of Smart Structures Technology to Rotorcraft SystemsJournal of the American Helicopter Society, 2000