Physics-Based Modeling of Maneuver Loads for Rotor and Hub Design
Author:
Affiliation:
1. Department of Aerospace Engineering, University of Maryland, College Park, Maryland 20742-0001
2. Rotor Dynamics and Aeromechanics, Bell Helicopter Textron Inc., Fort Worth, Texas 76101-0482
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031843
Reference17 articles.
1. RajmohanN. “Application of Hybrid Methodology to Rotors in Steady and Maneuvering Flight,” Ph.D. Thesis, School of Aerospace Engineering, Georgia Inst. of Technology, Atlanta, GA, 2010.
2. Rotor Airloads Prediction Using Loose Aerodynamic/Structural Coupling
3. Revolutionary Physics-Based Design Tools for Quiet Helicopters
4. Prediction and Analysis of Main Rotor Loads in a Prescribed Pull-Up Maneuver
5. Prediction of Helicopter Maneuver Loads Using a Fluid-Structure Analysis
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