Development and Implementation of Rotorcraft Preliminary Design Methodology using Multidisciplinary Design Optimization

Development and Implementation of Rotorcraft Preliminary Design Methodology using Multidisciplinary Design Optimization

A formal framework is developed and implemented in this research for preliminary rotorcraft design using IPPD methodology. All the technical aspects of design are considered including the vehicle engineering, dynamic analysis, stability and control, aerodynamic performance, propulsion, transmission...

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Bibliographic Details
Main Author: Khalid, Adeel S.
Format: Others
Language:en_US
Published: Georgia Institute of Technology 2007
Subjects:
All at Once
Aeronautical design standards
Blade element theory
Contributing analyses
Concurrent engineering
Collaborative optimization
Design structure matrix
Fixed point iteration
Genetic algorithms
Global sensitivity equation
Multidisciplinary design analysis
Multidisciplinary design optimization
Optimizer based decomposition
Overall evaluation criteria
Request for proposal
Response surface equation
Simultaneous analysis and design
Sequential quadratic programming
System sensitivity analysis
Total quality management
Online Access:http://hdl.handle.net/1853/14013

Internet

http://hdl.handle.net/1853/14013

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