Thermal Process Physics of ABE and LENR

Abstract

This paper is devoted to united conservation laws of mass, momentum and energy for thermal processes in air breathing engines (ABE) and simulation of low energy nuclear reactions (LENR). The united conservation laws are defined by intensive interaction of gaseous medium and thermal radiation. Here one of the famous items of thermodynamic simulation connects with introducing of external space thermostat with temperature T=2.73 K. Any studied technical system has a thermal contact with the space thermostat and may have some dissipation its energy. In our modeling a radiate dynamics is described as motion of a continuous lightly movable medium with help of the “field” functions and the Euler variables. We analyze basic designing complexities of high temperature turbo and jet engines related to origin of so-called "unexpected" heat of working process. Our approach allows proposing a simulation of low energy nuclear reactions and an analysis of the internal structures of electron, proton, neutron and nuclei with their particle thermodynamics.