ASPECTS CONCERNING THE CHARACTERISTICS OF THE
LAYER LIMIT THE HEAT SHIELD AT THE ROCKET MOTORS
The work addresses the results of recent research on the influence of
the characteristics of the layer thermal limit on energy yields of the motors
missile.
Keywords: gas jet, thermal boundary layer, engine rocket, nozzle, heat
transfer, Reynolds number
Cuvinte cheie: jet de gaze, strat limită termic, motor rachetă, ajutaj,
transfer termic, număr Reynolds
