Engineering Transactions, 39, 2, pp. 207-219, 1991

An Estimate of the Influence of the Compressor Stability Margin on the Thrust of a Turbojet Engine

M. Orkisz
Air Force Academy, Dęblin

The relations derived in the paper make it possible to analyze. the influence of the compressor stability margin upon the thrust of a turbo jet engine. The engines operating within the economy range (minimum fuel consumption) and optimum range (maximum thrust) are considered.

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