Gregory A. Wrenn

发表

Multidisciplinary Design Integration Methodology for a Supersonic Transport Aircraft

P. G. Coen, Augustine R. Dovi, Gregory A. Wrenn, 1995 .

Application of multidisciplinary optimization methods to the design of a supersonic transport

P. G. Coen, Augustine R. Dovi, Gregory A. Wrenn, 1992 .

Multilevel/multidisciplinary optimization scheme for sizing a transport aircraft wing

Augustine R. Dovi, Gregory A. Wrenn, A. Dovi, 1987 .

Aircraft design for mission performance using nonlinear multiobjective optimization methods

Augustine R. Dovi, Gregory A. Wrenn, A. Dovi, 1989 .

Multidisciplinary design integration system for a supersonic transport aircraft

P. G. Coen, Augustine R. Dovi, Gregory A. Wrenn, 1992 .

Supersonic transport wing minimum weight design integrating aerodynamics and structures

P. G. Coen, Augustine R. Dovi, Gregory A. Wrenn, 1994 .

Techniques for Aircraft Conceptual Design for Mission Performance Comparing Nonlinear Multiobjective Optimization Methods

Augustine R. Dovi, Gregory A. Wrenn, 1992 .

Integrating aerodynamics and structures in the minimum weight design of a supersonic transport wing

Peter G. Coen, Augustine R. Dovi, Gregory A. Wrenn, 1992 .

Multilevel Decomposition Approach to the Preliminary Sizing of a Transport Aircraft Wing

Augustine R. Dovi, Gregory A. Wrenn, A. Dovi, 1988 .

Development of an Inertia Relief Method for Aircraft with Dissimilar Engines in LEAPS

Bryce L. Horvath, Gregory A. Wrenn, 2021, AIAA AVIATION 2021 FORUM.

An indirect method for numerical optimization using the Kreisselmeir-Steinhauser function

Gregory A. Wrenn, G. Wrenn, 1989 .

A new algorithm for general multiobjective optimization

Jaroslaw Sobieszczanski-Sobieski, Augustine R. Dovi, Gregory A. Wrenn, 1988 .