A computational methodology for designing an experimental test matrix is presented based on the concept of potential and repulsive fields. The problem consists in the optimal distribution of test points in a two-dimensional domain, pursuant to hard constraints (permitted boundaries of the domain) and soft constraints (minimization of potential). Each test point is assumed to be the source of different fields which expose all other points to repulsive forces, thus accelerations, acting in different directions. The result of the mutual repulsive forces is a dynamic evolution of the configuration of test points in the domain, which eventually converges to a condition of minimum potential. An iterative process is adopted to find a numerical sol...
Although much progress has been achieved in the predictive capa- bilities of modern finite element c...
Through the use of difference equations and matrix notation a systematic procedure is developed for ...
In order to study the dynamical characters of aircraft landing gear and carry out successive optimiz...
A computational methodology for an experimental design problem based on the concept of potential and...
In this paper we present a computational methodology to solve the problem of the proper design of th...
In this paper we present a computational methodology to solve the problem of the proper design of th...
Planning test points for highly constrained flight tests is a lengthy and iterative process which re...
In this paper we study the problem of the design of the test matrix for an envelope expansion test c...
This paper initially describes an innovative approach to product realization called Knowledge Based ...
Planning test points for highly constrained flight tests is a lengthy and iterative process which re...
This paper describes an optimization algorithm for replicating a desired stress state of an aeroelas...
This paper proposes a new approach to force balance structural optimization featuring a computationa...
A specific feature of aircraft and spacecraft flight modes is related to difficulties of obtaining i...
Due the fact that aircraft structures work in an environment with lots of dynamic forces, it is of v...
A new technique was developed for designing optimal flight test inputs for aircraft parameter estima...
Although much progress has been achieved in the predictive capa- bilities of modern finite element c...
Through the use of difference equations and matrix notation a systematic procedure is developed for ...
In order to study the dynamical characters of aircraft landing gear and carry out successive optimiz...
A computational methodology for an experimental design problem based on the concept of potential and...
In this paper we present a computational methodology to solve the problem of the proper design of th...
In this paper we present a computational methodology to solve the problem of the proper design of th...
Planning test points for highly constrained flight tests is a lengthy and iterative process which re...
In this paper we study the problem of the design of the test matrix for an envelope expansion test c...
This paper initially describes an innovative approach to product realization called Knowledge Based ...
Planning test points for highly constrained flight tests is a lengthy and iterative process which re...
This paper describes an optimization algorithm for replicating a desired stress state of an aeroelas...
This paper proposes a new approach to force balance structural optimization featuring a computationa...
A specific feature of aircraft and spacecraft flight modes is related to difficulties of obtaining i...
Due the fact that aircraft structures work in an environment with lots of dynamic forces, it is of v...
A new technique was developed for designing optimal flight test inputs for aircraft parameter estima...
Although much progress has been achieved in the predictive capa- bilities of modern finite element c...
Through the use of difference equations and matrix notation a systematic procedure is developed for ...
In order to study the dynamical characters of aircraft landing gear and carry out successive optimiz...