Determination of Cycle Configuration of Gas Turbines and Aircraft Engines by Optimization Procedure
Keyword(s):
This paper is devoted to the analyses and optimization of simple and sophisticated cycles, particularly for various gas turbine engines and aero-engines (including scramjet engine) to achive the maximum performance. The optimization of such criteria as thermal efficiency, specific output and total performance for gas turbine engines, and overall efficiency, non-dimensional thrust and specific impulse for aero-engines have been performed by the optimization procedure with multiplier method. The comparisons of results with analytical solutions establishes the validity of the optimization procedure.
1991 ◽
Vol 113
(1)
◽
pp. 100-105
◽
Keyword(s):
Keyword(s):
2000 ◽
Vol 122
(4)
◽
pp. 680-684
◽
Keyword(s):
Keyword(s):
Keyword(s):
Keyword(s):
Keyword(s):
2000 ◽
Vol 12
(11)
◽
pp. 585-592
◽