Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Augustine R. Dovi"'
Publikováno v:
Journal of Aircraft. 32:290-296
An aircraft early preliminary design system that demonstrates the methodology for multidisciplinary communications and couplings between several engineering disciplines is described. A primary benefit of this system is the flexibility to demonstrate
Publikováno v:
Journal of Aircraft. 31:330-338
An approach is presented for determining the minimum weight design of aircraft wing models which takes into consideration aerodynamics-structure coupling when calculating both zeroth-order information needed for analysis and first-order information n
Autor:
Gregory A. Wrenn, Augustine R. Dovi
Publikováno v:
Journal of Aircraft. 27:1043-1049
A new technique which converts a constrained optimization problem to an unconstrained one where conflicting figures of merit may be simultaneously considered was combined with a complex mission analysis system. The method is compared with existing si
Publikováno v:
8th Symposium on Multidisciplinary Analysis and Optimization.
A new framework consisting of distributed objects for rapid multidisciplinary analysis is developed and applied to a high-speed civil transport configuration. The framework is based on the Common Object Request Broker Architecture (CORBA), a specific
Publikováno v:
4th Symposium on Multidisciplinary Analysis and Optimization.
An aircraft preliminary design system which provides the multidisciplinary communications and couplings between several engineering disciplines is described. A primary benefit of this system is to demonstrate advanced technology multidisciplinary des
Publikováno v:
AIAA Journal. 23:1775-1782
A method for decomposing an optimization problem into a set of subproblems and a coordination problem that preserves coupling between the subproblems is described. The decomposition is achieved by separating the structural element optimization subpro
Autor:
Gregory A. Wrenn, Augustine R. Dovi
Publikováno v:
Journal of Aircraft. 25:632-638
A multilevel/multidisciplinary optimization scheme for sizing an aircraft wing structure is described. A methodology using nonlinear programming in application to a very large engineering problem is presented. This capability is due to the decomposit
Publikováno v:
29th Structures, Structural Dynamics and Materials Conference.
Described is a new technique for converting a constrained optimization problem to an unconstrained one, and a new method for multiobjective optimization based on that technique. The technique transforms the objective functions into goal constraints.
Autor:
Augustine R. Dovi, Gregory A. Wrenn
Publikováno v:
28th Structures, Structural Dynamics and Materials Conference.