Theory and design of a gas turbine. Mikhaltsev V.E., Molyakov V.D.

Methods of calculating and designing turbines as part of modern and promising aircraft, stationary, transport gas turbine engines and combined installations.

are shown methods of optimizing the steps of turbines and multi -stage turbines in order to obtain the maximum importance of the efficiency in the framework of the restricted restrictions By the mass, size, the number of steps, depending on the location of the turbine as part of gas turbine engines.

The methods for determining the loss of energy and characteristics of turbines in aviation, energy, transport and combined engines in various operating modes.

For students of 4-6 courses of specialties "Aviation gas turbine engines", "stationary and transport engines based on aviation engines" and "non-traditional and renewable energy sources".