Multidisciplinary Design Optimization for Aeromechanics and Handling Qualities
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 20742
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.7943
Reference20 articles.
1. Helicopter vibration reduction using structural optimization with aeroelastic/multidisciplinary constraints - A survey
2. Integrated multidisciplinary design optimization of rotorcraft
3. Recent Applications of Design Optimization to Rotorcraft-A Survey
4. Optimum aeroelastic design of helicopter rotors for longitudinal handling qualities improvement
5. Efficient Treatment of Moderate Amplitude Constraints for Helicopter Handling Qualities Design Optimization
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