Jacques Peter

发表

CONCURRENT OR SIMULTANEOUS PLANNING OF SERVICE CHANGES: THE PARIS- LILLE EXPERIENCE.

Jacques Peter, 1999 .

Two-Dimensional Aerodynamic Optimization Using the Discrete Adjoint Method with or without Parameterization

Jacques Peter, Manuel Bompard, G. Carrier, 2011 .

A Fully-Nested Interpolatory Quadrature Based on Fejér's Second Rule

Jacques Peter, J. Peter, 2014, Curves and Surfaces.

Analysis of finite-volume discrete adjoint fields for two-dimensional compressible Euler flows pdf

Florent Renac, Jacques Peter, Cl'ement Labb'e, 2020, ArXiv.

Gradient-Based Aerodynamic Optimization with the elsA Software

Jacques Peter, Gerald Carrier, Antoine Dumont, 2014 .

Gradient-Based Optimization of CRM Wing-alone and Wing-body-tail Configurations by RANS Adjoint Technique

Jacques Peter, Gerald Carrier, Antoine Dumont, 2016 .

Unstructured mesh adaptation for functional outputs. With application to two dimensionnal invscid flows

Jean-Antoine Désidéri, Jacques Peter, J. Désidéri, 2016 .

Mesh quality assessment based on aerodynamic functional output total derivatives

Jean-Antoine Désidéri, Matthieu Meaux, Jacques Peter, 2014 .

Aerodynamic Shape Optimization of Hovering Rotors Using a Discrete Adjoint of the Reynolds-Averaged Navier–Stokes Equations

A. Le Pape, Jacques Peter, Antoine Dumont, 2011 .

Finite-volume goal-oriented mesh adaptation for aerodynamics using functional derivative with respect to nodal coordinates

Jean-Antoine Désidéri, Jacques Peter, Giovanni Todarello, 2016, J. Comput. Phys..

NON-INTRUSIVE STOCHASTIC STUDIES FOR EXTERNAL AND INTERNAL FLOWS USING THE elsA SOFTWARE

Jacques Peter, Antoine Fourmaux, Marc Lazare, 2010 .

Analysis of finite-volume discrete adjoint fields for two-dimensional compressible Euler flows

Florent Renac, Jacques Peter, Cl'ement Labb'e, 2022, J. Comput. Phys..

Sensitivity Analysis of a Strongly Coupled Aero-Structural System Using Direct and Adjoint Methods

Jacques Peter, Gerald Carrier, Meryem Marcelet, 2008 .

Large stencil viscous flux linearization for the simulation of 3D compressible turbulent flows with backward-Euler schemes

Jacques Peter, J. Peter, Frédérique Drullion, 2007 .

Goal oriented mesh adaptation using total derivative of aerodynamic functions with respect to mesh coordinates – With applications to Euler flows

Jacques Peter, Maxime Nguyen-Dinh, Pierre Trontin, 2012 .

Sensitivity analysis of a strongly coupled aero-structural system using the discrete direct and adjoint methods

Jacques Peter, Gerald Carrier, Meryem Marcelet, 2008 .

Goal oriented mesh adaptation using total derivative of aerodynamic functions with respect to mesh coordinates

Jacques Peter, Maxime Nguyen-Dinh, Pierre Trontin, 2011 .

Sensitivity analysis of a coupled aero-structural system using direct differentiation and adjoint equations

Jacques Peter, Gerald Carrier, Meryem Marcelet, 2006 .