On the Conservation Laws in the Optimal Control Problem for Laminar Boundary Layer of Non-equilibrium Dissociating Gas
Author(s):
Natalya Grigorievna Bilchenko
Candidate of Science in Physics and Mathematics
Researcher of Research Laboratory #16,
Department of Heat Engineering and Power Engineering Machinery,
Kazan National Research Technical University (KNRTU-KAI)
named after A. N. Tupolev.
bilchnat@gmail.com
Abstract:
The problems of mathematical modeling of optimal heat protection
of permeable surfaces of hypersonic aircraft
in non-equilibrium dissociating gas are considered.
The group theory approach to the optimization
of systems with distributed parameters is applied.
Conservation laws on all operators of the group admissible
by a system of nonlinear differential equations of parabolic type
are constructed.
Keywords
- conservation law
- first integral
- heat and mass transfer
- hypersonic flows
- infinitesimal operator
- laminar boundary layer
- Lie group
- non-equilibrium dissociation
- optimal control
References:
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