Add to ORKGA method for the optimization of structures to satisfy flutter velocity constraints is presented along with a method for determining the flutter velocity. A method for the optimization of structures to satisfy divergence velocity constraints is included
One way to increase the aircraft fuel efficiency is to reduce structural weight while maintaining ad...
Several minimum-mass optimization problems are solved to evaluate the effectiveness of a variety of ...
Design procedures for aircraft wing structures with control surfaces are presented using multidiscip...
Numerical analysis of derivatives of flutter velocity of aircraft structures to determine optimizati...
Using the first and the second derivative of flutter velocity with respect to the parameters, the ve...
A numerical procedure was developed for minimizing the structural mass of an aircraft structure whic...
Computational aspects of (1) flutter optimization (minimization of structural mass subject to specif...
The efficient design of aircraft structure involves a series of compromises among various engineerin...
The research reported in this thesis is concerned with the structural weight optimization of aircra...
Structural optimization with a flutter constraint for a vehicle designed to fly in the transonic reg...
Two analytical flutter solution approaches have been developed to optimize two and three dimensional...
"The influences of structural and aerodynamic modeling on the flutter analysis and multidisciplinary...
A design process which incorporates the object-oriented multidisciplinary design, analysis, and opti...
This preliminary investigation introduces the use of the Regier number as a flutter constraint crite...
Results of a study of the development of flutter modules applicable to automated structural design o...
One way to increase the aircraft fuel efficiency is to reduce structural weight while maintaining ad...
Several minimum-mass optimization problems are solved to evaluate the effectiveness of a variety of ...
Design procedures for aircraft wing structures with control surfaces are presented using multidiscip...
Numerical analysis of derivatives of flutter velocity of aircraft structures to determine optimizati...
Using the first and the second derivative of flutter velocity with respect to the parameters, the ve...
A numerical procedure was developed for minimizing the structural mass of an aircraft structure whic...
Computational aspects of (1) flutter optimization (minimization of structural mass subject to specif...
The efficient design of aircraft structure involves a series of compromises among various engineerin...
The research reported in this thesis is concerned with the structural weight optimization of aircra...
Structural optimization with a flutter constraint for a vehicle designed to fly in the transonic reg...
Two analytical flutter solution approaches have been developed to optimize two and three dimensional...
"The influences of structural and aerodynamic modeling on the flutter analysis and multidisciplinary...
A design process which incorporates the object-oriented multidisciplinary design, analysis, and opti...
This preliminary investigation introduces the use of the Regier number as a flutter constraint crite...
Results of a study of the development of flutter modules applicable to automated structural design o...
One way to increase the aircraft fuel efficiency is to reduce structural weight while maintaining ad...
Several minimum-mass optimization problems are solved to evaluate the effectiveness of a variety of ...
Design procedures for aircraft wing structures with control surfaces are presented using multidiscip...