J.-F. M. Barthelemy

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 .

Automatic Differentiation as a tool in engineering design

J.-F. M. Barthelemy, L. E. Hall, 1992 .

Multidisciplinary design integration system for a supersonic transport aircraft

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

A comparison of polynomial approximations and artificial neural netsas response surfaces

J.-F. M. Barthelemy, William C. Carpenter, W. Carpenter, 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 .

Engineering Applications of Heuristic Multilevel Optimization Methods

J.-F. M. Barthelemy, J. M. Barthelemy, 1989 .

Active damping of modal vibrations by force apportioning. [for spacecraft structures]

J.-F. M. Barthelemy, W. L. Hallauer, W. Hallauer, 1980 .

Sensitivity of modal-space control to nonideal conditions

J.-F. M. Barthelemy, W. L. Hallauer, W. Hallauer, 1981 .