Decomposition-based optimization procedure for high-speed prop-rotors using composite tailoring
- 1 September 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 32 (5), 1026-1033
- https://doi.org/10.2514/3.46832
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Multilevel decomposition procedure for efficient design optimization of helicopter rotor bladesAIAA Journal, 1995
- A DESIGN OPTIMIZATION PROCEDURE FOR MINIMIZING DRIVE SYSTEM WEIGHT OF HIGH SPEED PROP-ROTORSEngineering Optimization, 1995
- DESIGN OF HIGH SPEED PROPROTORS USING MULTIOBJECTIVE OPTIMIZATION TECHNIQUESEngineering Optimization, 1994
- A simulated annealing technique for multiobjective optimization of intelligent structuresSmart Materials and Structures, 1994
- Optimal locations of actuators for statistical static shape control of large space structure - A comparison of approachesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Formulation and Evaluation of an Analytical Model for Composite Box‐BeamsJournal of the American Helicopter Society, 1991
- Selected design issues of some high speed rotorcraft conceptsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Method for nonlinear optimization with discrete design variablesAIAA Journal, 1989
- Optimization by Simulated AnnealingScience, 1983
- A General Theory of Strength for Anisotropic MaterialsJournal of Composite Materials, 1971