Theory and Design of Rocket Engines

The physico-mathematical descriptions of the processes are presented: ignition, heat and mass transfer, non-stationary, turbulent and unstable combustion of fuel, gas terminalomics of heterogeneous and homogeneous combustion products, methods of mathematical modeling of energy characteristics and parameters of the workflow for non-stationary and quasistationary mode of operation of rocket engines of various purposes. Methods of calculating the loss of the specific pulse of traction, the scattering of the main parameters of the workflow and the method of selecting the system of control system of the vehicle of the aircraft. Mathematical models and methods for calculating the design and gas-dynamic parameters of rocket-direct-flow air jet engines are presented. For students, graduate students and teachers of universities relevant specialties