Reducing the Sonic Boom under a Supersonic Jet
 Gradient of the Sonic Boom objective function on the skin of the plane |
Area: Computational Fluid Dynamics
This work was done in collaboration with Dassault Aviation, who provided the simplified geometry of their supersonic business jet. This work was partly supported by the Comite d'Orientation Supersonique of the French Ministry for Research.
Related AD-Tool:
TAPENADE
Reference:
People involved:
Reference:
F. Courty, A. Dervieux, B. Koobus, L. Hascoët
Reverse automatic differentiation for optimum design: from adjoint state assembly to gradient computation
Article in Optimization Methods and Software, 2003
Laurent Hascoët, Mariano Vázquez, Alain Dervieux
Automatic Differentiation for Optimum Design, Applied to Sonic Boom Reduction
Conference proceeding, Computational Science and Its Applications -- ICCSA 2003, Proceedings of the International Conference on Computational Science and its Applications, Montreal, Canada, May 18--21, 2003. Part II, Springer, 2003
Reverse automatic differentiation for optimum design: from adjoint state assembly to gradient computation
Article in Optimization Methods and Software, 2003
Laurent Hascoët, Mariano Vázquez, Alain Dervieux
Automatic Differentiation for Optimum Design, Applied to Sonic Boom Reduction
Conference proceeding, Computational Science and Its Applications -- ICCSA 2003, Proceedings of the International Conference on Computational Science and its Applications, Montreal, Canada, May 18--21, 2003. Part II, Springer, 2003
People involved:
- F. Courty
- A. Dervieux
- L. Hascoet
- B. Koobus
- M. Vazquez