Methods of optimal gas turbine engine design at initial design stages
Aerospace propulsion engineering
Аuthors*, **, , ***,
Samara National Research University named after Academician S.P. Korolev, 34, Moskovskoye shosse, Samara, 443086, Russia
AbstractGas turbine engine initial-stage design tasks are examined. Examples of bypass engine optimization for long-range aircraft are given in two variants: without gas generator restrictions and with a given gas generator. The examples of parameters selection for gas turbine power-plant and gas turbine locomotive are given.
Keywords:gas turbine engine; optimization; design process; parameters selection; engine control